研究業績 - chubu-univ · 2014-05-13 · computational fluid dynamics, edited by g.de vahl davis...

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研究業績

[原著論文]

1.

S.Uchida, Y.Nakamura

On the Potential Theory of Distributed Singularities and its Edge Condition for a Lifting Flow of

Three-Dimensional Body

Memo. Fac. Eng., Nagoya Univ., 26, 2(1974), 183-208

2.

中村佳朗

非一様断面円管内の旋回流の解析

日本航空宇宙学会誌, 24, 273(1976), 490-496

3.

中村佳朗, 近藤継男, 内田茂男

流線解析法とその旋回流への応用

日本航空宇宙学会誌, 25, 278(1977), 139-144

4.

中村佳朗, 内田茂男

非一様断面円管内の旋回流の解析（第２報）

日本航空宇宙学会誌, 25, 281(1977), 283-288

5.

S.Uchida, Y.Nakamura, Y.Taniguchi

Analytical Solutions of Swirling Flow with an Arbitrary Distribution of Velocities along the Axis -Exact

Solutions

Trans. Japan Soc. Aero. Space Sci., 20(1977), 75-86

6.

内田茂男, 中村佳朗、中村治夫, 末広文雄, 坪井淳

レーザー流速計による旋回流の測定

日本航空宇宙学会誌, 25, 286(Nov. 1977), 510-517

7.

中村佳朗、中村治夫, 末広文雄, 坪井淳、内田茂男

レ－ザー流速計による管内旋回流の崩壊に関する実験

日本航空宇宙学会誌, 25, 287(Dec. 1977), 588-593

8.

Yoshiaki Nakamura

An Analysis of the Viscous Swirling Flow in a Cylindrical Tube

Trans. Japan Soc. Aero. Sci., 22(1979), 90-103

9.

Yoshiaki Nakamura and Shigeo Uchida

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A Contribution to the Occurrence of Axisymmetric Type of Vortex Breakdown,

Trans. Japan Soc. Aero. Space Sci., 23(1980), 79

10.

Yoshiaki Nakamura and Shigeo Uchida

Calculations of Axisymmetric Swirling Flows by the use of Parabolic Type Equations

Comput. Fluids, 9(1981), 463-467

11.

Yoshiaki Nakamura, Shigeo Uchida and Fumio Suehiro

Numerical Calculations of Swirling Flows in a Circular Pipe


12.

Y.Nakamura and S.Uchida

Breakdown Conditions of an Axisymmetric Swirling Flow

AIAA J., 19(1981), 1083-1085.

13.

Y.Nakamura, S.Uchida, and H.Kawazoe

A Calculation of Parabolic Type Equations for Axisymmetric Swirling Flows

Trans. Japan Soc. Aero. for Space Sci., 24(1982) 205

14.


Numerical Solutions of the Navier-Stokes Equations for Axisymmetric Weak Swirling Flows in a Pipe


15.

Y.Nakamura, A.Leonard, and P.R.Spalart

Vortex Simulation of an Inviscid Shear Layer

AIAA Paper, 82-0948,1982, pp. 1-14.

16.

Y.Nakamura, T.Hama, and M.Yasuhara

Axisymmetric Inviscid Swirling Flows Produced by Bellmouth and Centerbody

AIAA Journal, 20, 1982, pp. 561-562.

17.

S.Uchida, T.Kondo, and Y.Nakamura

Swirl Flow Studies in Diffusers Using the Flux Numerical methods in Analysis method

with Orthogonal Curvilinear Coordinates

International Journal for Numerical Methods in Engineering,

Vol.18, Issue 9, Sep. 1982, pp.1385-1399.

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18.


Numerical Simulation of Vortex Breakdown by the Vortex-Filament Method

AGARD CP 342(1983), 27.

19.

S.Uchida, Y.Nakamura, and M.Ohsawa

Experiments on the Axisymmtric Vortex Breakdown in a Swirling Air Flow

Trans. Japan Soc. Aero. Space Sci., 27(1985), 206-216.

20.


Vortex Breakdown Simulation

AIAA Paper, 85-1581(1985).

21.

石黒満津夫、中村佳朗、保原充

二次元翼まわりの非圧縮性流れ

第３回航空機計算空気力学シンポジウム論文集、航空宇宙技術研究所特別資料、SP-5, (1985), 217.

22.

S.Uchida and Y.Nakamura

Stability and Breakdown of Vortex Flow

Recent Studies on Turbulent Phenomena, edited by T.Tatsumi et al., Association for Science Documents Info

rmation, (1985), 163.

23.

Y.Nakamura and Y.Takemoto

Solutions of Incompressible Flows Using a Generalized QUICK Method

Numerical Methods in Fluid Dynamics II, edited by K.Oshima, Japan Society of Computational Fluid

Dynamics (1985) 285.

24.

Y.Takemoto and Y.Nakamura

A Three-Dimensional Incompressible Flow Solver

Lecture notes in Physics Springer-Verlag, 264(1986) 594.

25.

石黒満津夫、中村佳朗、保原充

ψ－ω法による非圧縮性流れの数値解析

流体熱工学研究、21(1986) 47.

26.

片岡卓也、中村佳朗、保原充

ナビエ・スト－クス方程式による３次元鈍頭物体まわりの超音速流の計算

流体熱工学研究、21(1986) 55.

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27.

Y.Takemoto, H.Yamabe, Y.Abe, I.Minami, and Y.Nakamura

A Curvilinear Coordinate Method for the Solutions of Incompressible Navier-Stokes Equations Using theThir

d- Order Upwind Difference Scheme

農業土木学会論文集、121(1986) 241.

28.


Internal Structure of a Vortex Breakdown

AIAA Paper, 86-1074(1986).

29.

S.Uchida, Y.Nakamura, J.Z.Zhang, and N.Sagawa

An Experiment on a Spiral Type of Vortex Breakdown of the Swirling Flow Produced in a Pipe

Trans. Japan Soc. Aero. Space Sci., 30(1987), 38-44.

30.

Y.Nakamura

Periodical Distribution of Vortices with Finite Core

Trans. Japan Soc. Aero. Space Sci., 30(1987)45-54.

31.


Several Approaches to the Study of Vortex breakdown

Proc. of 2nd Colloquium on Vortex Breakdown, the Deutsche Forshungsgemeinschaft (1987) 115.

32.

保原充、中村佳朗

PNS 方程式による超音速流れの計算

第５回航空機計算空気力学シンポジウム論文集、航空宇宙技術研究所特別資料、 SP-8, (1987), 43-48.

33.

Y.Nakamura and M.Yasuhara

Numerical Simulation of Incompressible Flow around Three-Dimensional Wing

Computational Fluid Dynamics, edited by G.de Vahl Davis at al., North-Holland, (1988) 785.

34.


Solutions of Circular- Sectioned Pipe Flows Using a Three-Dimensional Generalized Quick Method

Computational Fluid Dynamics edited by G.de Vahl Davis et al., North-Holland (1988), 703.

35.

Y.Nakamura, M.Yasuhara, K.Kuwabara, and W.Jia

Incompressible Flow through Multiple Passages

AIAA/ASME/SIAM/APS 1st National Fluid Dynamics Congress, 3(1988), July 1693

36.

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保原充、中村佳朗、王健平

スペクトル法による極超音速流れの計算

(Computations of the hypersonic flow by the spectral method)

日本航空宇宙学会誌、36, 419（１９８８）, pp. 542-549.

37.


Numerical Simulation of 2-D and 3-D Channel Flows Using a 3rd-Ordered Accurate Generalized QUICK

Scheme

Proc. of the Third International Symposium on Refined Flow Modelling and Turbulence Measurements,

edited by Y.Iwasa et al., (1983) 53.

38.

M.Yasuhara, Y.Nakamura, and J.P.Wang

Numerical Calculation of Hypersonic Flow by the Spectral Method

Lecture Notes in Physics Springer-Verlag, No. 323, (1988) 607-611.

39.

保原充、中村佳朗、稲垣伸二

有翼飛翔体まわりの高速流の計算計算

第６回航空機計算空気力学シンポジウム論文集、航空宇宙技術研究所特別資料、SP-9, (1988), 151. 4

40.

Y.Nakamura and M.Yasuhara

Numerical Simulation of Incompressible Flows

Proc. of Soviet Union- Japan Symposium on Computational Fluid Dynamics, edited by P.I.Chushkin et al.,T

he USSR Academy of Sciences, 1(1989), pp.88.

41.

M.Yasuhara and Y.Nakamura

On Numerical Simulation of Compressible Flows

Proc. of Soviet Union- Japan Symposium on Computational Fluid Dynamics, edited by P.I.Chushkin et al.,

The USSR Academy of Sciences, 1, 1989, pp. 7.

42.

賈為、中村佳朗、保原充、桑原宏成

スラット・フラップ翼まわりの流れの計算

日本航空宇宙学会誌、３７,428、 (1989)、430-440.

43.

J.Tanaka, Y.Nakamura, and M.Yasuhara

A Comparison among Three DSMC Methods

Trans. Japan Soc. Aero. Space Sci.,32, 97(1989), pp. 116-128.

44.

M.Yasuhara, Y.Nakamura, and J.Tanaka

Monte Calro Simulation of Flow into Channel with Sharp Leading Edges

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Progress in Astronautics and Aeronautics, 118 (1989), 582-596.

45.

Y.Nakamura, S.Inagaki, and M.Yasuhara

A Hypersonic Flow in a Channel with Sharp Leading Edges

AIAA Paper-89-1841.

46.

W.Jia, Y. Nakamura and M.Yasuhara

Incompressible Flow through Multiple Passages

Numerical Heat Transfer, 16, December 1989, 451-465.

47.

J.Tanaka, Y.Nakamura, and M.Yasuhara

A Problem on Time Counter in the DSMC Method

Proc. of the International Symposium on Computational Fluid Dynamics-Nagoya, Japan Society of

Computational Fluid Dynamics, (1989) 513-518.

48.

W.Jia, Y.Nakamura, and M.Yasuhara

Numerical Simulation of Incompressible Flows


Computational Fluid Dynamics (1989) 683.

49.

J.P.Wang, Y.Nakamura, and M.Yasuhara

Several Improvements of Spectral Method in Compressible Flow Calculation


Computational Fluid Dynamics (1989) 1210.

50.

A.E.Sakya, Y.Nakamura, and M.Yasuhara

A Preliminary Study of Transonic Flow around NACA0012

第７回航空機計算空気力学シンポジウム論文集、航空宇宙技術研究所特別資料、SP-10, (1989), 255.

51.

賈為、中村佳朗

自然対流を伴う流れの数値計算法

流体熱工学研究 24(1989) 41

52.

中村佳朗、賈為、保原充

ψ－ωを用いた非圧縮性流計算法の改良

日本航空宇宙学会誌、38, 437, 1990, pp.309-320.

53.


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ｕ－ｖ－ｐ法による自然対流の数値計算法

ながれ、9, 1（１９９０）34-52.

54.

王健平, 中村佳朗, 保原充

スペクトル選点法による圧縮性ナビエ・スト－クス方程式の高精度計算

(Accurate Computations of Compressible Navier-Stokes Equations by the Spectral Collocation Method)

日本航空宇宙学会誌、38, 436 （1990）, 232-240

55.

W.Jia, Y.Nakamura, M.Yasuhara

A Flow around Airfoil with Slat and Flap

AIAA-90-1535 (1990)

56

Y.Nakamura, J.P.Wang, M.Yasuhara

A Calculation of the Compressible Navier-Stokes Equations in Generalized Coordinates by the Spectral Met

hod

Lecture Notes in Physics, Springer-Verlag, No. 371, 1990, 127-131

57


ノイマン条件を持つ圧力ポアソン方程式の新しい数値計算法

日本航空宇宙学会誌、38, 441(1990) 541-550

58.

M.Yasuhara, Y.Nakamura, and J.Tanaka

DSMC Simulation of Supersonic Flow past 2-Dimensional Body

Proc. of 17th International Symposium on Rarefied Gas Dynamics(1990)

59.

Y.Suzuki, Y.Nakamura, and M.Yasuhara

A Hypersonic Flow over a Flat Plate at M=8

Proc. of the second Japan-Soviet Union Joint Symposium on Computational Fluid Dynamics,

II (1990), 14-21.

60.

J.P.Wang, Y.Nakamura, and M.Yasuhara

A Chebyshev Collocation Method for the Compressible Navier- Stokes Equations

in Generalized Coordinates

Trans. Japan Soc. Aero. Space Sci., 33, 101 (1990) pp.120-134

61.

武本行正、山辺春雄、中村佳朗

一般化座標Ｋ～ε乱流モデルによる２次元場の流れシミュレーション

四日市大学論集 2(1990) 129.

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62.

M.Yasuhara, Y.Nakamura, K.Tsuboi, and K.Kuwabara

Theory and Shock Tunnel Experiments on Flow past Hypersonic Vehicles

Memoirs of the Faculty of Engineering, Nagoya University

42, 2, 1990, 290-359.

63.

M.Yasuhara, Y.Nakamura, and W.Jia

A Comparison between Computation and Experiment for Flows around Airfoil with Flap and Slat

Trans of Japan Soc. Aero. Space Sci., 33, 102, 1991, pp. 218- 233.

64.

城之内忠正、中村佳朗、保原充、辻村直久

電磁流体方程式への風上差分法の適用

日本航空宇宙学会誌、39, 451, 1991, 403-409.

65.

T.Nagashima, Y.Nakamura, M.Yasuhara, and K.Tsuboi

Shock Interaction Induced by Two Hemisphere-Cylinders

IPAC, SAE P-246, 1991, pp. 581-589.

66.

Y.Nakajima, Y.Nakamura, and M.Yasuhara

Flow Field around Thick Delta Wing with Rounded Leading Edge

IPAC, SAE P-246, 1991, pp. 393-404.

67.

W. Jia and Y. Nakamura

A New Formulation for Incompressible Viscous Flows

Computational Fluid Dynamics '92, Edited by Ch.Hirsch et. al., Elsevier, 1992, 383-390.

68.

Y. Nakamura, Y. Nakajima, and W. Jia

Aerodynamic Characteristics of Thick Delta Wing

Fluid Dynamics of High Angle of Attack, The IUTAM Symposium Tokyo, Japan Sep. 13-17, Eds. R.Kawamu

ra et al., Springer-Verlag, September 1992, pp.375-382.

69.

A.E.Sakya and Y.Nakamura

An Improvement of RNG Based Algebraic Turbulence Model

Transactions of the Japan Society for Aeronautical and Space Sciences, 35, 108, 1992, 43-55.

70.

賈為、中村佳朗

非圧縮性流に対するｖ－ｑ法とψ－ｑ法

第１０回航空機計算空気力学シンポジウム論文集、航空宇宙技術研究所特別資料 SP-19, 1992, pp.135-140.

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71.

W.Jia and Y.Nakamura

A Numerical Procedure to Solve Viscous Flow around Arbitrary Moving Bodies

13th International Conference on Numerical Methods in Fluid Dynamics, 1992, Rome

Lecture Notes in Physics No. 414, Springer-Verlag, 1992, 225-229.

72.


A New Formulation for Incompressible Viscous Flows

Computational Fluid Dynamics '92, Proc. First European Computational Fluid Dynamics Conference,

Elsevier, 1992, 383-390.

73.

中村佳朗

イオン化の化学反応と磁場を含む流れ

機械の研究、養賢堂、45, 1,1992, 217-219.74.

74.

A.E.Sakya, Y.Nakamura, and M.Yasuhara

Evaluation of an RNG Based Algebraic Turbulence Model

Computers & Fluids, 22, 2/3, March/May, 1993, 207-214.

75.

中村佳朗, 賈為, 水野大介

任意に運動する物体周りの非圧縮性流れの計算法

日本航空宇宙学会誌, 41, 469, 1993, 96-103.

76.

S.Atsuchi, Y.Nakamura, and H.Kawazoe

A Study on Aerodynamic Sound Generated by Interaction of Jet and Plate

AIAA Paper 93-3118, 1993, 1-10.

77.


The Three-Dimensional v-q Method for Incompressible Viscous Flows

11th AIAA Computational Fluid Dynamics Conference,

AIAA Paper 93-3341-CP, 1993, 490-500.

78.

M.Zahar, 中村佳朗、中島、小野

厚いデルタ翼の総圧分布について

流体熱工学研究、東海流体熱工学研究会、28, 1, 1993, 15-25.

79.

J.P. Wang, Y.Nakamura, and M.Yasuhara

Global Coefficient Adjustment Method for Chebyshev Collocation Method and its Application to

Compressible Navier-Stokes Equations

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Journal of Computational Physics, 107, 1, July 1993, 160-175.

80.


Incompressible Viscous Flows around Arbitrarily Moving Bodies subject to Surface Deformation

Proc. of 5th International Symposium on Computational Fluid Dynamics-Sendai, August 1993, pp. 99-104.

81.

Y.Nakamura and A.E.Sakya

Capturing of Transition by the RNG Based Algebraic Turbulence Model

Proc. of 5th International Symposium on Computational Fluid Dynamics-Sendai

August 1993, pp. 109-116

82.

H.Kawazoe, S.Atsuchi, Y.Nakamura, and A.Ochi

An Aerodynamic Sound due to Interaction of Jet Shear with Plate Edge

AIAA paper 93-4393, 1993, 1-7.

83.

保原充、中村佳朗

風洞実験と数値実験－飛翔体初期研究の経験から

日本航空宇宙学会誌、41,475, 1993, pp.439-444.

84.

M.Yasuhara, Y.Nakamura, J.Tanaka

Unified Plots of Hypersonic Flow past Flat Plates in Transition Regime

Rarefied Gas Dynamics: Space Science and Engineering,

Progress in Astronautics and Aeronautics, AIAA, Vol. 160, 1993, pp.229-233.

85.

M.Ishiguro, Y.Nakamura, M.Shimizu, H.Kawazoe

Flow Separation inside Conical Nozzle of an Arc Heated Wind Tunnel,

AIAA Ground Testing Conference, AIAA paper 94-2594, 1994, pp. 1-8.

86.

A.Urita, Y.Nakamura and H.Kawazoe

A Measurement of Freely Oscillating Body Subject to Aerodynamic Forces

AIAA Ground Testing Conference, AIAA paper 94-2612, 1994, pp. 1-8.

87.

H.Kawazoe, Y.Nakamura, T.Ono, and Y.Ushimaru

Static and Total Pressure Distributions around a Thick Delta Wing with Rounded Leading Edges

AIAA 25th Fluid Dynamics Conference, Colorado Springs, AIAA paper 94-2321, 1994, pp.1-12.

88.

川添博光、中村佳朗、厚地聡

空力音発生に関する実験的研究-自由噴流と平板エッジによる音と流れ場の計測-

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流体熱工学研究、東海流体熱工学研究会、第２９巻、第１号、1994, pp.45-56.

89.

A.Ochi, H.Kawazoe, and Y.Nakamura

A Simulation of Axisymmetric Jet on Networked EWS

Parallel Computational Fluid Dynamics: New Algorithms and Applications,

N.Satofuka, J.Periaux and A.Ecer (Editors),1995,

Elsevier Science B.V., pp. 385-392.

(Proc. of Parallel CFD '94 Kyoto, 1994, pp. 385-392.)

90.

I.S.Men'shov and Y.Nakamura

An Extension of Multidimensional Riemann Problems and its Application to Godunov's Method

第１２回航空機計算空気力学シンポジウム論文集、航空宇宙技術研究所特別資料, SP-27, 1994, pp.105-110.

91.

Casamara and Y.Nakamura

振り子運動する物体の空気力による減衰過程のシミュレ－ション

第１２回航空機計算空気力学シンポジウム論文集、航空宇宙技術研究所特別資料, SP-27, 1994, pp.321-326.

92.


The ψ-q formulation and boundary condition for incompressible flows in multi-connected region

Proc. of 14th ICNMFD, Bangalore, India, 1994, edits. S.M.Deshpande et al., Springer-Verlag,

pp.195-200 July.

93.

A.E.Sakya and Y.Nakamura

An Application of the RNG Based Algebraic Turbulence Model to Aerodynamic Characteristics

Transactions of the Japan Society for Aeronautical and Space Sciences, 37, 116, 1994, 75-95.

94.

石黒満津夫、川添博光、中村佳朗、小原正徳

高エンタルピ－気流のノズル内部流特性について

流体熱工学研究、東海流体熱工学研究会、第２９巻、第２号、 1994, pp.11-19.

95.

H.Kawazoe, Y.Nakamura, M.Ohara, N.Hamamoto, N.Arai, and K.Kitagawa

Spectroscopic Study of High Enthalpy Flow around a Blunt Body in Arc-heated Wind Tunnel

Proc. of International Symp. on Advanced Energy Conversion System and Related Technologies, 1994,

71-78.

96.

Y.Nakamura and Andi Eka Sakya

Capturing of Transition by the RNG Based Algebraic Turbulence Model

Computers & Fluids, 24, 8, Nov. 1995, 909-918.

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97.

川添博光、中村佳朗

空力音発生における非圧縮ジェットせん断層の役割

日本航空宇宙学会誌、43, 493, 1995(Feb), pp. 586-592

96.

I.Nakamori and Y.Nakamura

An Upwind Scheme Based on the Flux-Vector Splitting Method

33rd Aerospace Sciences Meeting and Exhibit, Reno,

AIAA paper 95-0471, 1995, pp. 1-7.

97.

石黒満津夫、中村佳朗

ノズル内における高エンタルピ－気流の電離特性に関する実験的考察

日本航空宇宙学会誌、43, 501, 1995, pp. 586-592

98.

H.Kawazoe, Y.Nakamura, and Y.Ikeda

Effects of Reynolds and Mach Numbers on Sound Generation in Jet Shear Flow with Plate Edge

Inserted

Proc. of First Joint CEAS/AIAA Aeroacoustics Conference, Munich, Germany, June 1995

CEAS/AIAA-95-069, I, 525-534.

99.

I.Nakamori and Y. Nakamura

An Upwind Scheme for Inviscid and Viscous Hypersonic Flow

AIAA CFD Conference, San Diego

AIAA paper 95-1732, June 1995, pp.971-980.

100.

H.Kawazoe, Yoshiaki Nakamura, and Y. Ushimaru

Dynamic Analysis of Thick Delta Wing with Arbitrary Motion in Wind Tunnel

AIAA paper 95-2268, 1995, 1-13

101.

Yoshiaki Nakamura and Eiji Kobayashi

Effect of Compressibility on Free Shear Layer of Axisymmetric Jet

The Recent Developments in Turbulence Research,

International Academic Publishers,

Proc. Of SINO-JAPAN Workshop of Turbulent Flows,

edited by Zhang,Z.S. and Miyake,Y., 1995, 218-228.

102.

A. Ochi, Y.Nakamura, H.Kawazoe

A New Domain Decomposition Method Using Virtual Sub-domain

Proc. of Parallel CFD' 95, California Institute of Tech.

Pasadena, CA, June 1995, pp.26-28.

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103.

中森一郎、中村佳朗

平板に入射する衝撃波により増大する熱流束の数値解析

流体熱工学研究、30, 1, 1995, 93-102.

104.

Y.Nakamura, H.Kawazoe, E.Kobayashi

Vortex Dynamics in Compressible Jet and its Effect on Aerodynamic Sound

The 1995 ASME/JSME Fluids Engineering and Laser Anemometry Conference and Exhibition,

Hilton Head Island, SC, August 13-18, 1995.

High Speed Jet Flows -1995-, FED-Vol.214, 1995, pp.71-76.

105.

I.Nakamori, Y.Nakamura

Heat Transfer Calculation of Rocket Booster Using the Multi- Domain Method

Proc. of 6th ISCFD, Lake Tahoe, Vol. II, 1995, 873-878.

106.

I. Men'shov and Y.Nakamura

An Implicit Advection Upwind Splitting Scheme for Hypersonic Air Flows in Thermochemical

Nonequilibrium

Proc. of 6th ISCFD, Lake Tahoe, Vol II, 1995, 815-820.

107.

瓜田明, 中村佳朗, 坪井淳, 稲谷芳文

再突入物体まわりの遷音速流れ

日本航空宇宙学会誌, 43, 503, 1995, 696-706.

108.

I.Maeda and Y.Nakamura

Effect of Compressibility on Boundary Layer Fluctuations

Proc. of Int. Symp. on Mathematical Modelling of Turbulent Flows, edited by

H.Daiguji and Y.Miyake, Tokyo, 1995, 13-18.

109.

Y.Nakamura and I.Maeda

Growth of Three Dimensional Disturbance in Compressible Jet

Proc. of Int. Symp. on Mathematical Modelling of

Turbulent Flows, edited by H.Daiguji and Y.Miyake, Tokyo, 1995, 19-24.

110. I.Men’shov and Y.Nakamura

Implementation of the LU-SGS Method for an Arbitrary Finite Volume Discretization,

第９回数値流体力学シンポジウム論文講演集、1995, pp. 123-124.

110.

崔長壽、杉山善幸、中村佳朗、楠本吉昭

- 14 -

翼端すきまのある翼に対するポテンシャル流非線形解析

日本航空宇宙学会誌、44, 508, 1996, 314-321.

111.

H.Kawazoe, Y.Nakamura, N.Hamamoto and M.Ohara

Number Density Measurement of Excited Argon Gas around a Blunt Body

34th Aerospace Sciences Meeting & Exhibit,

AIAA paper 96-0229, 1996, 1-11.

112.

石黒満津夫、中村佳朗

電離を考慮した高エンタルピ－ノズルの設計

日本航空宇宙学会誌, 44, 507, 1996, 227-233.

113.

T.Ohara, Y.Nakamura, H.Kawazoe and Y.Tanahashi

Flow Field of Three Dimensional Shock-Boundary Interaction

Proc. of 20th International Symposium on Space Technology and Science, Gifu, Japan

May 19-25, 1996, 96-n-23, pp. 1-6.

114.

Y.Nakamura and T.Narahara

Fluctuation Characteristics Produced by Vortex Breakdown

AIAA paper 96-2078, 1996, 1-14.

115.


Incompressible Flow Solver of of Arbitrarily Moving Bodies with Rigid Surface

JSME International Journal, Series B, 39, 2, May 1996, 315-325.

116.


球頭円錐円柱周りの遷・超音速流れの特性

日本航空宇宙学会誌、44, 510, 1996, 416-422.

117.

瓜田明、中村佳朗

鉛直流中で振り子運動する再突入物体の圧力分布

日本航空宇宇宙学会誌、44, 515, 1996(12), 729-734.

118.

M.G.Lee, Y.Nakamura, A.Ochi and P.R.Lahur

An Unstructured Grid around Supersonic Transport (SST)

Proc. of Third ECCOMAS Computational Fluid Dynamics Conference, 1996, 10.

119.

I.Maeda, Y.Nakamura, H.Kawazoe, A.Ochi and T.Narahara

- 15 -

Natural Convection Flow Simulated on Workstation Cluster

Proc. of Parallel CFD '96, Capri, Italy, 1996.

120.

Y.Nakamura and I.Maeda

Spatially Developing Compressible Jet

Proc. of 5th Russia-Japan Joint Symposium on Computational Fluid Dynamics,

Novosibirsk, Russia, 1996, 6-8.

121.

H.Ebneddin Hamidi and Y.Nakamura

Unsteady Measurement of Pressure Distribution around Oscillating Body

流体熱工学研究、31, 1, 1996, pp. 61-72.

122.

Y.Nakamura, I.Maeda

Three-Dimensional Mechanism of Disturbance Growth in Compressible Jet

Proc. of 2nd Asia workshop on Computational Fluid Dynamics, edited by H.Kubota,

1996, 85-90.

123.

Yoshiaki Nakamura and Ichiro Maeda

Disturbance Evolution in Compressible Boundary Layer

Proc. of 2nd China-Japan Workshop on Turbulent Flows,

edited by Q.D.Wei, Beijing, 1996, 22-27.

124.

前田一郎, 中村佳朗

空間発展圧縮性ジェットの数値シミュレ－ション

流体熱工学研究、31, 2, 1996, pp. 31-40.

125.

Naoki Hamamoto, Hiromitsu Kawazoe, Yoshiaki Nakamura, N.Arai, and K.Kitagawa

Spectroscopic Study of High Enthalpy Flow around a Blunt Body in Arc-heated Wind Tunnel

J. of Energy Conversions and Management, 38, 10-13, July 1997, pp. 1177-1186.

126.


圧縮性境界層における擾乱の発達の数値解析

ながれ、16, 1 Feb. (1997) pp. 59-67.

127.


高次精度計算法による空間発展圧縮性ジェットの解析

ながれ、16, 3 June(1997) pp.271-282.

128.

- 16 -

Y.Tanahashi, T.Ohara, and Y.Nakamura

Three Dimensional Shock/Boundary Layer Interaction Between a Rocket and SRB

AIAA paper 97-2572 June 1997, pp.1-11

129.

N.Hamamoto, M.G.Lee, Y.Nakamura, and I.Men'shov

Heat Transfer Calculation of Blunt Bodies in Nonequilinrium Air Flows

AIAA paper 97-2055, pp. 1 -11, 1997

130.

上野真, 中村佳朗

ロ－ル運動するデルタ翼の空力動特性

流体熱工学研究、32, 1, 1997, pp. 27-34.

131.

N.Hamamoto, Y.Nakamura

Spectroscopic Study of Arc-heated, High-speed Nitrogen Flow before a Blunt Body,

Proc. of International Conference on Fluid Engineering, JSME, Centennial Grand Congress

July 1997, pp. 989-994.

132.

H.E.Hamidi, Y.Nakamura

Control of a Falling Body with a Mathematical Model for Unsteady Aerodynamic Force

Transactions of the Japan Society for Aeronautical and Space Sciences,

40, 129, Nov. 1997, pp. 207-220.

133.

坪内修, 中村佳朗

噴流火炎の並列計算

流体熱工学研究, 32, 2, Dec.1997, 35-42

134.


圧縮性正方形ジェットの数値シミュレ－ション

日本航空宇宙学会誌, 46, 529, 1998(2月), 111-119

135.

N.Hamamoto, Y.Nakamura, T.Suzuki

Spectroscopic Study of Arc- heated Nonequilibrium Nitrogen Flow before a Blunt Body,

AIAA Paper 98-2944, June 1998, 1-8

136.

H.Yamaguchi and Y.Nakamura

Optimization of Low Boom Configuration of SST by Genetic Algorithm

AIAA Paper 98-2899, June 1998, 1-9

137.

- 17 -

M.Ueno, T.Matsuno, and Y.Nakamura

Unsteady Aerodynamics of Rolling Thick Delta Wings with High Aspect Ratio,

AIAA Paper98-2520, June 1998, pp. 226-234

138.


Synthesis of a Falling Body Controller with Modeling Error of Aerodynamic Force


41, 131, May 1998, pp. 19-28.

139.

H.Yamaguchi and Y.Nakamura

Optimization of Forebody Shape for Reducing Sonic Boom

Proc. of ECCOMAS 98, Computational Fluid Dynamics ’98 edited by K.D.Papailiou et al.,

John Wiley & Sons, Sep. 1998, pp. 570 - 574.

140.


Implementation of the Semi-Lagrangian Scheme for Incompressible Navier-Stokes Equations

Proc. of the Sixth Japan-Russia Sympo. on Computational Fluid Dynamics,

Sep. 1998, pp.165-168.

141.

坪内修中村佳朗

動的移動境界法を用いた噴流拡散火炎の並列計算

日本機械学会論文集（Ｂ編）

64, 626, 1998-10, pp. 324-330.

142.

Y.Nakamura and H.Yamaguchi

Breakdown of Compressible Jet and its Aeroacoustic Emission

Proc. of the 3rd China-Japan Workshop on Turbulent Flows, 31 Oct.-4 Nov.,

Edited by LIAN Qixiang and KIYA Masaru, Beijing, 1998, pp.140-146.

143.

Ebneddin Hamidi, Y.Nakamura and Y.Takizawa

A New Flow Visualization Method Using Liquid Nitrogen and Laser Sheet

Proc. of VSJ-SPIE98, International Conference on Optical Technology and Image

Processing in Fluid, Thermal, and Combustion Flow,

CD version, AB147, Dec. 1998.

144.


Falling Body Controller Design Using Nonlinear Inverse Dynamics

AIAA Paper 99-0895, Jan. 1999, pp. 1-10.

145.

- 18 -

P.R.Lahur and Y.Nakamura

A New Method for Thin Body Problem in Cartesian Grid Generation

AIAA Paper 99-0919, Jan. 1999, pp.1-8.

146.

坪内修、中村佳朗

触媒フラットバーナの燃焼特性

日本機械学会論文集、Ｂ編、６５、６３２、 Apr. 1999, pp.1467-1472.

147.

M.Kaneko and Y.Nakamura

Effects of Shock Wave/Boundary Layer Interaction on Reservoir Temperature in Shock Tunnel

AIAA Paper 99-3529, June, 1999

148.


A New Flow Visualization Method Using Condensation of Water Vapor in Air Flow


149.

T. Layukallo and Y.Nakamura

The Efficiency of a Second Throat in Stabilizing the Flow in a Transonic Wind Tunnel


150.

棚橋美治、栗田充、中村佳朗

極超音速鈍頭物体の底面部圧力におけるジェット干渉効果

日本航空宇宙学会誌、47、546、(July)1999, pp. 291-297.

151.

Hiromitsu Kawazoe, Yoshiaki Nakamura and Yoshiyuki Ikeda (2)

Prediction of Sound Generation from Flow Field of Axisymmetric Jet with

Circular Plate Edge Inserted in the Shear Layer

Proc. of the 3rd ASME/JSME Joint Fluids Engineering Conference,

July 18-23, 1999, San Francisco, California

FEDSM99-7235

pp. 1-6.

151.

Yoshiaki Nakamura and Hayato Yamaguchi

Compressible Jet and its Sound Emission

Computational Fluid Dynamics Journal, 8, 2, (July)1999, pp. 250-256.

152.

棚橋美治、栗田充、中村佳朗

亜・遷音速流中におけるジェット干渉による鈍等物体底面部での圧力分布特性

日本航空宇宙学会誌、47、547、(August)1999, pp. 306-313.

- 19 -

153.

Y. Tanahashi, T. Ohara, and Y. Nakamura

Three-Dimensional Shock/Boundary-Layer Interaction Between a Rocket and a Booster,

J. Spacecraft and Rocket, 36, 5, September-October, 1999, pp. 681-687.

154.

片岡拓也、中村佳朗

自動車車室内温度分布解析に基づいた乗員の温冷感予測

日本機械学会論文集（Ｂ編）、６５巻、６４０号、１９９９－１２、pp.232-239.

155.

M.K.Ibrahim and Y.Nakamura,

The Effects of Vane-Type Tabs on Flow and Acoustic Fields of Supersonic Jet

AIAA Paper 2000-0087, Reno, January, 2000, pp.1-10.

156.

Takashi Matsuno and Yoshiaki Nakamura

Self-Induced Roll Oscillation of 45-Degree Wings


157.

Igor MEN’SHOV and Yoshiaki NAKAMURA

Variation Matrices in the Riemann Problem with Application to Implicit Godunov’s Method


158.

坪内修、中村佳朗、Mohamed RAMEEZ

熱交換器のある場合の触媒フラットバーナの基礎特性

日本機械学会論文集（Ｂ編）、６６巻、６４５号、２０００－５、pp.253-260.

159.

Taku Furukawa and Yoshiaki Nakamura

Shock-boundary Layer Interaction in Annular Flow

Proc. of ISCFD’99, Computational Fluid Dynamics Journal, Special Number, 2001, pp.339-344.

160.

Yoshiaki Nakamura and Taku Furukawa

Sound Emission from an Under-expansion Jet

Proc. of ISCFD’99, Comput. Fluid Dynamics Journal, 9, 1, 2000, pp.568-573.

161.

Igor Men’shov and Yoshiaki Nakamura

On Implicit Godunov’s Method with Exactly Linearized Numerical Flux,

Computers and Fluids, 29, 6, April 2000, pp. 595-616.

162.

- 20 -


Numerical Simulations and Experimental Comparisons for High Speed Nonequilibrium Air Flows,

Fluid Dynamics Research Journal, 27, 5, Nov. 2000, pp. 305-334.

163.

Paulus R. Lahur and Yoshiaki Nakamura

A Cartesian Grid Generation Method Considering a Complicated Cell Geometry at the Body Surface


43, 139, May 2000, pp. 8-15.

164.


高速流計算における高解像度流束分離法

日本航空宇宙学会誌

48, 557, June, 2000, pp. 167-172.

165.

M.K. Ibrahim and Y. Nakamura

Flow Field and Noise Charactersitics due to Supersonic Jet Shear Layer-Vortex Interaction,

AIAA Paper 2000-2533, June, 2000, pp. 1-11.

166.

I. Men’shov and Y. Nakamura:

A Godunov-type Method for Computational Acoustics,

AIAA Paper 2000-2329, June 2000, pp. 1-10.

167.

M.Kaneko, I. Men’shov and Y. Nakamura

Reflected Shock Wave/Boundary Layer Interaction in High-Enthalpy Shock Tunnel,


168.

Paulus R. Lahur and Yoshiaki Nakamura

Anisotropic Cartesian Grid Adaptation


169.

T.Matsuno, S.Yokouchi and Y. Nakamura

The Effect of Leading-Edge Profile on Self-induced Oscillation of 45-Degree Delta Wings,

AIAA Paper 2000-4004, August 2000, pp. 1-10. (Bound volume of applied aerodynamics)

170.

Mitsuru Kurita, Tsuyoshi Inoue and Yoshiaki Nakamura

Aerodynamic Interaction due to Side Jet from a Blunted Cone in Hypersonic Flow

AIAA Paper 2000-4518, August 2000, pp. 833-841. (Bound volume of applied aerodynamics)

171.

- 21 -

Thombi Layukallo and Yoshiaki Nakamura

Flow Stabilization in a Transonic Wind Tunnel with a Second Throat,

Journal of Aircraft, 37, 6, November 2000, pp. 1033-1037.

172.

Munetsugu Kaneko and Yoshiaki Nakamura

Numerical Investigation of Unsteady Flow Field with Shock Interaction in Shock Tunnel

AIAA Paper 2001-0742, January 2001

173.

Mitsuru Kurita, Takumi Okada, and Yoshiaki Nakamura (4)

The Effects of Attack Angle on Aerodynamic Interaction due to Side Jet from a Blunted Body in a Superso

nic Flow, AIAA Paper 2001-0261, January 2001, pp. 1-10.

174.

T.Yamada, M.D.Mamun, and Y. Nakamura

Analysis and Control of the Flow Field around Spinning Flat Plate Wing, AIAA Paper 2001-0692, Jan. 2001,

pp. 1-13.

175.

Ibrahim, Mohammed Khalil and Yoshiaki Nakamura

Effects of Rotating Tabs on Flow and Acoustic Fields in Supersonic Jet

AIAA Journal, 39, 4, July 2001, pp. 745-748.

176.

Yoshiaki Nakamura and Taku Furukawa

Numerical Simulation of Sound Emission from Supersonic Jet

Computational Fluid Dynamics for the 21st Century, Springer-Verlag, 2001, pp. 350-365.

177.

M.Kurita, T.Okada, and Y.Nakamura

The Effects of Attack Angle on Side Jet Aerodynamic Interaction in a Blunted Body at Hypersonic Flow

AIAA Paper 2001-1825, April 2001, pp. 1-18.

178.

Paulus R. Lahur and Yoshiaki Nakamura (2)

Anisotropic Cartesian Grid Adaptation


44, 143, May 2001, pp. 29-38.

179.


A New Numerical Scheme for Computational Aeroacoustics Based on the Solution to the Variational Rieman

n Problem, AIAA Paper 2001-2627, June 2001, pp. 1-10.

180.

Paulus R. Lahur and Yoshiaki Nakamura (6)

- 22 -

Simulation of Flow around Moving 3D Body on Unstructured Cartesian Grid, AIAA Paper 2001-2605, June 2001, pp.1-9.

181.

Mohammed K. Ibrahim, Ryoji Kunimura, and Yoshiaki Nakamura

Spreading Enhancement of Axisymmetric Supersonic Jet by the Use of Micro Jets, AIAA Paper 2001-3048, June 2001, p

p. 1-15.

182.

Takeshi KAIDEN and Yoshiaki NAKAMURA

Numerical Analysis of Aerodynamic Control by Micro-flap around Delta Wing, AIAA Paper 2001-1441, 2001, pp. 1-12.

183.

Munetsugu Kaneko, Igor Men’shov, and Yoshiaki Nakamura

Numerical Simulation of Nonequilibrium Flow in High-Enthalpy Shock Tunnel with EIH Scheme, AIAA Paper 2001-2860,

June 2001, pp. 1-11.

184.

濱本直樹、中村佳朗

高速非平衡窒素流における球頭物体澱み流線上の振動・回転温度

日本航空宇宙学会論文集

49, 574, November, 2001, pp. 375-381.

185.


Anisotropic Cartesian Grid Adaptation, Computational Fluid Dynamics 2000, edited by Prof.N.Satofuka, Springer, 2001,

pp.73-78.

186.

Igor Men’shov and Y.Nakamura

An Accurate Method for Computing Propagation of Sound Waves in Non-Uniform Moving Fluid, Computational Fluid Dy

namics 2000, edited by Prof. N. Satofuka, Springer, 2001, pp.549-554.

187.

Igor Men’shov, Yoshiaki Nakamura and Alexandr Severin

An Adaptive Method for Compressible Flows on Anisotropic Nested-type Grids, Proc. of ISCFD’99, Comput. Computation

al Fluid Dynamics Journal, Special Number, 2001, pp.517-527.

188.


Flow Calculation of Moving Body on Cartesian Grid by Using New Cell-Merging Method


44, 145, Nov. 2001, pp. 171-178.

188.

Munetsugu Kaneko, Igor Men’shov and Yoshiaki Nakamura

Computation of Nozzle Starting Process with Thermal and Chemical Nonequilibrium in High-Enthalpy Shock Tunnel, AI

AA Annual Meeting, AIAA Paper 2002-0142, pp. 1-10, January 2002

- 23 -

189.

T. Yamada and Y.Nakamura

Aerodynamic Characteristics of a 65-deg Delta Wing at Steep Spin, AIAA Paper 2002-0097 January 2002, pp.1-9.

190.

D. Azuma and Y. Nakamura

Lift Enhancement of a Thick Delta Wing Using Rotational Leading Edges, AIAA Paper 2002-0847, January 2002, pp. 1-

8.

191.

T.Matsuno, S.Yokouchi, and Y.Nakamura

Flow Control on a 45-Degree Delta Wing Using a Small Flap, AIAA Paper 2002-0558, January 2002, pp. 1-8.

192.

I. Men’shov and Y. Nakamura

Towards Implicit Godunov Method: Exact Linearization of the Numerical Flux, Godunov Methods: Theory and Applicatio

ns, Edited by E.F.Toro, Kluwer Academic/ Plenum Publishers, 2001, pp. 611-622.

193.

Thombi Layukallo, Daisuke Hayashi, and Yoshiaki Nakamura (5)

Passive Separation Control on a Body at Transonic Speed

Trans. Japan Soc. Aero. Space Sci.

Vol. 44, No. 146, Feb. 2002, pp. 229-237.

194.

山田貴史、一ノ瀬敬之、中村佳朗

スピンする平板翼の空力特性について


第50巻、第576号、Jan. 2002、pp.15-21.

195.


On Instability of Acoustic Waves Propagating in Stratified Vortical Flows

JSME International Journal

Series B, Vol. 45, No.1, Feb. 2002, pp. 79-84.

196.

Mohammed K. Ibrahim and Yoshiaki Nakamura

Correlation between Linear Stability Theory and Transition of Compressible Jet Shear Layer

Trans. Japan Soc. Aero. and Space Sci.,

Vol. 45, No. 147, May 2002, pp. 35-44.

197.

Mohammed K. Ibrahim, Ryoji Kunimura, and Yoshiaki Nakamura

Mixing Enhancement of Compressible jets by Using Unsteady Micro-jets as Actuator

AIAA J., Vol. 40, No. 4, 2002, pp.681-688.

- 24 -

198.

Munetsugu Kaneko, Igor Men’shov and Yoshiaki Nakamura

Numerical Study of Unsteady Shock Waves in Hypersonic Nozzle Flows, AIAA Paper 2002-3118, 2002.

199.

K.Doi, I. Men’shov and Y. Nakamura

Numerical Simulation of Interaction Between Moving Shock Wave and Solid Particle Layer, AIAA 32nd Fluid Dynamics

Conference, St. Louis, AIAA Paper 2002-3180, 2002.

200.


Numerical Simulation of Acoustic Waves Propagating in a Perfectly Expanded Jet Flow

Computational Fluid Dynamics Journal

Vo. 11, No.2, July 2002. pp. 178-184.

201.

栗田充、岡田拓巳、中村佳朗、本郷素行、稲谷芳文

超音速領域におけるサイドジェット空力干渉の迎角効果について

日本航空宇宙学会論文集, 50, 583, Aug. 2002, pp.310-317.

202.

T.Matsuno, S.Yokouchi, and Y.Nakamura

Small-Leading Edge Flap for Post-Stall Flow Control on a 45-deg Delta Wing, ICAS2002, ICAS 2002-8.3.3.

203.

Y.Nakamura and T.Yamada

Aerodynamic Charactersitics of Spin Phenomenon for Delta Wing, ICAS2002, ICAS 2002-8.8.3.

204.

栗田充、岡田拓巳、中村佳朗

極超音速鈍頭物体におけるサイドジェット空力干渉

日本航空宇宙学会論文集, 50, 585, Oct. 2002, pp.394-401.

205.


Implementation of the Variational Riemann Problem Solution for Calculating Propagation

Of Sound Waves in Nonuniform Flow Fields

Journal of Computational Physics, 182, 2002, pp. 118-148.

206.

栗田充、岡田拓巳、中村佳朗

衝撃風洞における感圧塗料計測法について

日本航空宇宙学会論文集, 51, 588, Jan. 2003, pp. 10-16.

- 25 -

207.

東大輔、中村佳朗

回転する前縁部によるデルタ翼の揚力増加

日本航空宇宙学会論文集, 51, 589, Feb. 2003, pp. 52-60.

208.

Thombi Layukallo and Yoshiaki Nakamura

Passive Separation Control on a Square Cylinder at Transonic Speed


Vol. 44, No. 150, Feb. 2003, pp. 236-242.

209.

Tetsuya Nakamura, Munetsugu Kaneko, Igor Men’shov and Yoshiaki Nakamura

Numerical Simulation on Aerodynamic Interaction between a Side Jet and Flow around a Blunt Body in Hypersonic Flo

w, AIAA Paper 2003-1135, Jan. 2003, pp.1-8.

209.

I.Menshov, Y.Nakamura

Abnormal Amplification of Sound Waves Refracted by an Oblique Shock Wave,

Abstracts of the 8th Japan-Russia Joint Symposium on Computational Fluid Dynamics,

Sendai, September 24-26, 2003, Ed. Nakahashi, pp. 100-101, 2003.

210.

Takashi Matsuno, Shigeru Yokouchi and Yoshiaki Nakamura

Data-Based Modeling of Non-Slender Wing Rock, AIAA Paper 2003-0738, Jan. 2003, pp.1-9.

211.

Yoshiaki Nakamura and Mitsuru Kurita

Pressure- and Temperature-Sensitive Paint Measurements in Shock Tunnel

Aerodynamics, Thermophysics, Thermal Protection, Flight System Analysis and Design of Asteroid

Sample Return Capsule,

ISAS Report SP No.17, March 2003, pp. 191-198.

212.

山田貴史、中村佳朗

スピンするデルタ翼の空力特性について


第51巻、第591号、April 2003、pp.133-140.

212.

Hashimoto Atsushi, Men’shov Igor and Yoshiaki Nakamura

Panel Flutter Analysis with a Fluid-Structure Coupled Scheme,

- 26 -

AIAA Paper 2003-3721, 33rd AIAA Fluid Dynamics Conference and Exhibits,

23-26 June 2003, Orlando, Florida, pp.1-10.

213.


A Composite Explicit-Implicit Godunov Method for Unsteady Problems on Highly Stiff Grids, Computational Fluid Dyna

mics 2002, Proc. of the second International Conference on Computational Fluid Dynamics, ICCFD, Sydney, Australia,

15-19 July 2002, Edited by S. Armfiels et al., pp. 479-484.

214.

海田武司、中村佳朗

超音速流中におけるマイクロフラップによるデルタ翼ローリングモーメント制御


第51巻、第596号、September 2003、pp. 506-511.

215.

K.Kitamura, T.Nakamura, I.Men’shov and Y.Nakamura

CFD Analysis of Aerodynamic Interference between a Delta Wing and a Hemisphere-Cylinder, AIAA Paper 2204-1378, R

eno, January 2004, pp.1-10.

216.

I.Menshov and Y.Nakamura

A Hybrid Explicit-Implicit, Unconditionally Stable Scheme for Unsteady Compressible Flows,

AIAA Journal, 42, 3, March 2004, 551-559.

217.

松野隆、横内滋、中村佳朗

45°デルタ翼の失速域におけるウイングロックの振動機構


第52巻、第601号、February 2004、pp. 80-86.

218.


デルタ翼後縁ジェットによる揚力増加

日本航空宇宙学会論文集, 52, 602, March 2004, pp. 108-113.

219.

金子宗嗣、メンショフ・イゴール、中村佳朗

衝撃波管における反射衝撃波と固体壁との干渉

日本航空宇宙学会論文集, 52, 603, April 2004, pp. 153-159.

220.

Jian-ping Wang, Yoshiaki Nakamura and Ting-wen Ji

Computation of Cavity Flow by Finite Element Method with

Finite Spectral Shape Function,

Computational Fluid Dynamics Journal, 12(4)73,

January 2004, pp. 601-605.

- 27 -

221.

金子宗嗣、メンショフ・イゴール、中村佳朗

境界層干渉を伴う非定常衝撃波伝播に対する高効率計算手法の開発

日本航空宇宙学会論文集, 52, 604, May 2004, pp. 196-202.

222.

海田武司、中村佳朗

遷音速流れにおける２次元楕円翼の抵抗および揚力変動の制御に関するＣＦＤ解析


第52巻、第604号、May 2004、pp. 227-234.

223.

Takeshi Kaiden and Yoshiaki Nakamura

Numerical Analysis of Aerodynamic Control of Delta Wing by Microflap

Journal of Aircraft, 41, 3, May-June 2004, pp. 555-563.

224.

Kimihito OBASE and Yoshiaki NAKAMURA

Aerodynamic and Aeroacoustic Interactions of a High-Speed jet with a Flat Plate, 2nd AIAA Flow Control Conference, 2

8 June to 1 July, Portland, Oregon, AIAA 2004-2404, 2004, pp. 1-10.

225.

Atsushi Hashimoto, Igor Men’shov and Yoshiaki Nakamura

Sound Emission from the Helical Mode of Supersonic Jet, AIAA Paper 2004-2656, June 2004, pp.1-12.

226.

Takao Saito, Tetsuya Nakamura, Munetsugu Kaneko and Yoshiaki Nakamura

Numerical Investigation of SRB Ignition Overpressure, AIAA 2004-2342, June 2004, pp.1-10.

227.

Kenichi Kitamura, Atsuhiro Nishino, Takahumi Ishikawa, Igor Men’shov and Yoshiaki Nakamura

A Device for Reduction of Heat Flux Produced by Hypersonic Shock Interference, AIAA 2004-2638, June 2004, pp. 1-13.

228.

西野敦洋、石川尊史、岡田拓巳、中村佳朗

極超音速におけるデルタ翼・球頭円柱間の空力干渉流れ場


第52巻、第606号、July 2004、pp. 289-294.

229.


45°デルタ翼におけるロール角に対する流れ場の不連続変化



230.

- 28 -


前縁ミニフラップによる45°デルタ翼のロール制御



231.

金子宗嗣、中村佳朗

衝撃風洞貯気槽温度に対する衝撃波／境界層干渉の影響


第53巻、第612号、January 2005、pp. 36-41.

232.

I.Menshov and Y.Nakamura

Instability of Isolated Compressible Entropy-Stratified Vortices

Physics of Fluids, 17, 2, 2005, pp.034102-1-034102-15.

233.

M.Kaneko, I.Mne'shov, Y.Nakamura

Numerical simulation of nonequilibrium flow in high-enthalpy shock tunnel

Energy, 30, 2005, pp. 165-179.

234.

土井克則、Igor Men’shov、中村佳朗

衝撃波流れによって形成される粉塵雲の数値シミュレーション

日本機械学会論文集（Ｂ編）、71巻、703号、2005-3、pp.760-765.

235.

濱本直樹、金子宗嗣、メンショフイゴール、中村佳朗

熱的・化学的非平衡を考慮した衝撃波・衝撃波干渉流の解析


第53巻、第617号、June 2005、pp. 241-247.

236.

Kenichi Kitamura, Igor Men’shov and Yoshiaki Nakamura

Shock/Shock and Shock/Boundary-layer Interactions in Two-Body Configurations, AIAA 2005-4893, June 2005, pp. 1-12.

237.


On Instability and Breakdown of Isolated Vortices, AIAA 2005-4674, June 2005, pp. 1-11.

238.

土井克則、Igor Men’shov、中村佳朗

衝撃波流れにより上昇する固体粒子の数値解析

日本機械学会論文集（Ｂ編）、71巻、708号、2005－8、pp. 30-34.

239.

山田貴史、堀地孝雄、中村佳朗

スピン状態の航空機模型における尾翼の効果について


第53巻、第618号、July 2005、pp. 241-247.

- 29 -

240.

西野敦洋、石川尊史、中村佳朗

超音速におけるデルタ翼・半球円柱間の空力干渉流れ場


第53巻、第621号、Oct. 2005、pp. 446-451.

241.

西野敦洋、石川尊史、北村圭一、中村佳朗

極超音速TSTO空力干渉場における２物体間隔の空力加熱率への影響


第53巻、第622号、Nov. 2005、pp. 503-509.

242.

加藤由博、メンショフ・イゴール、中村佳朗

非圧縮流れ場と音場に分離された方程式による円柱まわりの空力音の計算

日本機械学会論文集（Ｂ編）、71巻、711号、2005-11、pp. 82-89.

243.

M. Jones and Y.Nakamura

Azimuthal Vorticity Dynamics and Vortex Breakdown Above a Delta Wing, AIAA-2006-1309, pp.1-13, Jan. 2006.

244.


前縁回転／後縁ジェットハイブリッド法によるデルタ翼揚力増加


第54巻、第626号、March 2006、pp. 116-120.

245.


地面板上の角柱から発生する空力音の計算

日本機械学会論文集（Ｂ編）、72巻、716号、2006-4、pp.104-111.

246.

A. Hashimoto, Y.Furuta, N.Yagi and Y.Nakamura

Experimental and Numerical Investigation of Delta Wing Flutter in Low Subsonic Flow, AIAA-2006-3215, pp. 1-15, June

2006.

247.

Y.Kim, Y.Nakamura, and I.Men’shov

Effect of Nozzle Lip Shape on Screech Tone in Supersonic Jet, AIAA-2006-3706, June 2006, pp. 1-9.

248.

Dong Li, Igor Men’shov, and Yoshiaki Nakamura

Detached-Eddy Simulation of Three Airfoils with Three Different Stall Onset Mechanisms

Journal of Aircraft, 43, 4, July- August 2006, pp. 1014-1021.

- 30 -

249


Exact Flux Linearization for Convergence Improvement in the Implicit Godunov Method, Proc. of the Third Internationa

l Conference on Computational Fluid Dynamics, ICCFD3, Toronto, 12-16 July 2004, Computational Fluid Dynamics 2004,

Editors C.Groth and D.W.Zingg, Springer 2006, pp. 791-797.

250.


自動車のドアミラーから発生する空力音の計算

日本機械学会論文集（Ｂ編）、72巻、722号、2006-10、pp. 72-79.

(英語版)

Yoshihiro Kato, Igor Men’shov and Yoshiaki Nakamura

Aeroacoustics Simulations around Automobile Rear-View Mirrors

Journal of Fluid Science and Technology

Vol.3, No.7, 2008, pp. 892-905

251

Y.Ueno, K.Kawamura, Y.Nakamura

Numerical Simulation Based on CFD and Flight Dynamics for Morphing Body, AIAA-2007-73, January 2007.

252

M. Jones and Y.Nakamura

Dynamics of the Vortex Core during Pitching of a High-Sweep Delta Wing, AIAA-2007-1284, Jan. 2007, pp. 1-12.

253.

橋本敦、古田泰之、八木直人、中村佳朗

低速デルタ翼フラッタ現象における大変形振動流れ場の解析


第55巻、第637号、February 2007、pp. 104-110.

254.

橋本敦、八木直人、中村佳朗、伊藤博文、海田武司

曲面パネルの流体構造連成計算法によるフラッタ解析


第55巻、第638号、March 2007、pp. 150-155.

255.

Yannick Rousseau, Igor Men’shov and Yoshiaki Nakamura

Morphing-Based Shape Optimization in Computational Fluid Dynamics


Vol.50, No. 167, May 2007, pp. 41-47.

256.

K.Hanai, H.Ozawa and Y.Nakamura

Two-Stage-To-Orbit Booster Configuration for Reducing Aerodynamic Heating at Hypersonic Speed, AIAA-2007-4220, Jun

e 2007, pp.1-14.

- 31 -

257.

Y.S. Kim and Y.Nakamura

Characteristic Boundary Conditions with Finite-Volume ENO scheme for Aeroacoustic Simulations,

International Journal of CFD, International Journal of Computational Fluid Dynamics,

21, 1, 2007, pp. 1-10.

258.

北村圭一、森浩一、花井勝祥、矢橋務、小澤啓伺、中村佳朗

TSTOオービタ形状の超音速空力干渉流れ場への影響,日本航空宇宙学会論文集,第55巻、第646号、November 2007、pp. 509-515.

259.

土井克則、中村佳朗

衝撃波流れにより上昇する２固体粒子の数値解析,日本機械学会論文集（Ｂ編）、73巻、736号、2007－12、pp. 2410-2415.

260.

H.Ozawa, K.Hanai, K.Kitamura, K.Mori and Y.Nakamura

Experimetal Investigation of Shear-layer/Body Interactions in TSTO at Hypersonic Speed, AIAA-2008-723, January 2008,

pp.1-14.

261.

M.Miyoshi, T.Ishii, A.Hashimoto, K.Mori and Y.Nakamura

Computational Analysis of Parachute Motions Using the Immersed Boundary Method, AIAA-2008-0311, January 2008, p

p.1-10.

262.

小澤啓伺、花井勝祥、中村佳朗

傾斜前面円柱先頭形状によるTSTO超音速空力干渉の低減,日本航空宇宙学会論文集,第56巻、第648号、January 2008、pp. 8-14.

263.

橋本敦、小林貴広、中村佳朗

遷音速鈍頭２次元物体でのタブによるベース抵抗低減,日本航空宇宙学会論文集,第56巻、第648号、January 2008、pp. 15-21.

264.

Hiroshi OZAWA, Katsuhisa HANAI, Mohammed IBRAHIM, Koichi MORI and Yoshiaki NAKAMURA

Experimental Analysis of TSTO Aerodynamic Heating Problems at Hypersonic Speed, AIAA 2008-2671, Dayton, April 20

08, pp.1-8.

265.

Y.S. Kim and Y.Nakamura

Effect of Nozzle Lip Shape on Screech Tone in a Supersonic Jet, Trans. Japan Soc. Aero. Space Sci., Vol.51, No. 171,

May 2008, pp. 1-7.

266.

北村圭一、中村佳朗

極超音速衝撃波干渉流れにおける空力加熱の数値解析,日本航空宇宙学会論文集,第56巻、第653号、June 2008、pp. 269-277.

- 32 -

267.

北村圭一、小澤啓伺、花井勝祥、森浩一、中村佳朗

極超音速TSTOにおける衝撃波干渉・境界層剥離を伴う流れ場の解析,日本航空宇宙学会論文集,第56巻、第653号、June 2008、pp.

278-285.

268.

Keiichi KITAMURA, Yoshiaki NAKAMURA and Eiji SHIMA

An Evaluation of Euler Fluxes II: Hypersonic Surface Heating Computation, AIAA-2008-4275, Seattle, June 2008, pp.1-2

2.

269.

河村耕平、上野陽亮、中村佳朗

数値流体力学と数値飛行力学の連成に基づく竹とんぼのフライトシミュレーション,日本航空宇宙学会論文集,第56巻、第654号、J

uly 2008、pp. 324-330.

Kohei Kawamura, Yosuke Ueno and Yoshiaki Nakamura

Flight Simulation of Taketombo Based on Computational Fluid Dynamics and

Computational Flight Dynamics

Journal of the Japan Society for Aeronautical and Space Sciences

Vol.56. No. 654, 2008, pp. 324-330.

270.

Mohammed K. Ibrahim, Tetsuya Nakamura, Keiichi Kitamura, Koichi Mori and Yoshiaki Nakamura

The Role of Vortices in Side Jet/Blunt Body Interaction at Hypersonic Speed, Trans. Japan Soc. Aero. Space Sci., Space

Technology Japan (online), Vol. 7, January 2009, pp. 1-10.

271.

Hiroshi OZAWA, Koichi MORI and Yoshiaki NAKAMURA

Experimental Analysis of TSTO Aerodynamic Interactions Based on Oil Flow Patterns at Hypersonic Speed, AIAA 2009-

1286, Orlando, January 2009, pp.1-9.

272.

Mohammed K. IBRAHIM, Soichiro MATSUMOTO, Hiroshi OZAWA, Koichi MORI and Yoshiaki NAKAMURA

Visualization of Flow Field over Rotating Blades Using Pressure Sensitive Foil Technique, AIAA 2009-1076, Orlando, Ja

nuary 2009, pp.1-14.

273.

小澤啓伺、北村圭一、花井勝祥、三好理也、森浩一、中村佳朗

超音速空力干渉を利用したカプセル型宇宙輸送システムの緊急分離,日本航空宇宙学会論文集,第57巻、第664号、May 2009、pp. 1

75-182.

274.

上野陽亮、中村佳朗

空気力学と飛行力学に基づく鳥の飛行に関する数値シミュレーション


第57巻、第667号、August 2009、pp. 317-322.

- 33 -

275.

M.K.Ibrahim, T.Sawai, K.Obase, K.Mori and Y.Nakamura

Experimental Investigation of Screech-Tone Characteristics of Jet Interaction with a Flat Plate

AIAA Journal, 47, 9, September 2009, 2031-2038.

276.

Michael Jones, Atsushi Hashimoto and Yoshiaki Nakamura

Criteria for Vortex Breakdown Above High-Sweep Delta Wings,

AIAA Journal, 47, 10, October 2009, 2306-2320.

277.

三好理也、森浩一、中村佳朗

Immersed Boundary法を用いたパラシュート開傘課程の流体・連成シミュレーション


第57巻、第670号、November 2009、pp. 419-425.

278.

Atsushi Hashimoto, Takashi Aoyama and Yoshiaki Nakamura

Effects of Turbulent Boundary Layer on Panel Flutter

AIAA Journal, 47, 12, December 2009, 2785-2791.

279.

小澤啓伺、花井勝祥、北村圭一、森浩一、中村佳朗

極超音速衝撃波・境界層干渉におけるCrackの空力加熱への影響


第58巻、第674号、March 2010、pp. 68-75.

280.

Keiichi Kitamura, Eiji Shima, Yoshiaki Nakamura, and Philip R. Roe

Evaluation of Euler Fluxes for Hypersonic Heating Computations

AIAA Journal, 48, 4, April 2010, 763-776.

281.

Akio Ochi, M.K.Ibrahim and Yoshiaki Nakamura

Computational Fluid Dynamics Validation Study of Wake-Capturing

Capability for a Flat-Plate Wake

Journal of Aircraft, Vol.47, No.2, March-April 2010, pp. 441-449.

282.

Mohammed El-Ghandour, Mohammed K. Ibrahim, Koichi Mori and Yoshiaki Nakamura

Control of Leakage Flow by Triple Squealer Configuration in Axial Flow Turbine


Vol. 53, No. 179, May 2010, pp. 1-7.

283.

- 34 -

Hiroshi OZAWA, Keiichi KITAMURA, Katsuhisa HANAI, Koichi MORI and Yoshiaki NAKAMURA

Unsteady Aerodynamic Interaction between Two Bodies at Hypersonic Speed


Vol. 53, No. 180, August 2010, pp. 114-121.

284.

Mahmoud EL-GENDI, Mohammed K. IBRAHIM, Koichi MORI and Yoshiaki NAKAMURA

Novel Flow Control Method for Vortex Shedding of Turbine Blade


Vol. 53, No. 180, August 2010, pp. 122-129.

285.

汪運鵬、田中潤治、轟木峻、土井克則、中村佳朗

表面移動法によるフラップ表面の剥離流制御


第58巻、第679号、August 2010、pp. 239-244.

286

土井克則、川鍋健、濱本直樹、中村佳朗

気流中に置かれた三次元台状物体の表面上を移動する液滴群の数値シミュレーション

日本機械学会論文集（Ｂ編）、76巻、768号、2010－12、pp. 1134-1139.

286.

Koichi Mori, Yoshiki Murahashi, Yutaka Koga, Yoshiaki Nakamura, M.K.Ibrahim

and Takashi Takahashi,

Simple Technique for Precise Measurement of Transmission Loss of Planar Sound Waves

AIAA Journal, 48, 10, October 2010, 2377-2385.

287.

Mahmoud EL-GENDI, Katsunori DOI, Mohammed K. IBRAHIM, Koichi MORI

and Yoshiaki NAKAMURA

Comparison between Hot and Cold Flow Conditions of Turbine Cascade


Vol. 53, No. 181, November 2010, pp. 171-179.

288.

Mohammed El-Ghandour, Koichi MORI and Yoshiaki NAKAMURA,

Desensitization of Tip Clearance Effects in Axial Flow Turbines, J. of Fluid Science and

Technology, 5, 2, 2010, pp. 317-330.

289.

Mohammed El-GHANDOUR, Mohammed K. IBRAHIM, Katsunori DOI and Yoshiaki NAKAMURA,

Effects of Tip Cavity Depth, Width, and Location on the Leakage Flow in an Axial Turbine Cascade,

J. of Fluid Science and Technology, 5, 3, 2010, pp. 558-573.

- 35 -

290.

Mohammed K. IBRAHIM, Soichiro MATSUMOTO, Koichi MORI

and Yoshiaki NAKAMURA

Visualization of Pressure Field over Rotating Blades Using Pressure Sensitive Foil Technique


Vol. 53, No. 182, February 2011, pp. 243-249.

291.

横井宏尚、小澤啓伺、松本宗一郎、土井克則、中村佳朗

極超音速圧縮コーナ流れの境界層再付着とキャビティの干渉による空力加熱


第59巻、第690号、July 2011、pp. 169-175.

292.

土井克則、Mohd FADHLI、川島渉、中村佳朗

CFDを用いたブーメランの飛行シミュレーション


第59巻、第693号、October 2011、pp. 273-280.

293.

Wang,Y. and Nakamura,Y.

Supersonic Unsteady Flow around a Capsule-shaped Abort System with Angle of Attack,

International Journal of Aerospace and Lightweight Structures

Vol.1, No.1, 2011, pp. 133-142.

294.

Xiaopeng, Xue and Yoshiaki Nakamura

Computational Analysis of Supersonic Flexible Parachute Using Immersed Boundary Method,

International Journal of Aerospace and Lightweight Structures

Vol.1, No.2, 2011, pp. 283-299.

293.

香山寛人、汪运鵬、小澤啓伺、土井克則、中村佳朗

フェンスによる超音速空力干渉を利用したカプセル分離


第60巻、第2号、April 2012、pp. 74-79.

294.

Yunpeng WANG, Hiroshi OZAWA and Yoshiaki NAKAMURA

Numerical Investigation of Supersonic Oscillatory Flow over a Capsule-shaped Abort System


Vol. 55, No. 5, September 2012, pp. 286-294.

295.

Katsunori DOI, Masaya MIYOSHI, Naoki HAMAMOTO and Yoshiaki NAKAMURA,

Direct Numerical Prediction of Aerodynamic Noise Emitted from a Generic Automobile Rear-View

Mirror,

- 36 -

Journal of Fluid Science and Technology, 7, 3, 2012, pp. 290-303.

296.

横井宏尚、石橋孝介、香山寛人、中村佳朗

極超音速ランプ上のキャビティにおける仕切り板の空力加熱率への影響

航空宇宙技術、Vol.11, 2012, pp. 89-97.

297.

Yunpeng Wang, Hiroshi Ozawa, Hiroto Koyama, and Yoshiaki Nakamura

Abort Separation of Launch Escape System Using Aerodynamic Interference

AIAA Journal, 51, 1, January 2013, 271-276.

298.

Hironao YOKOI, Hiroto KOYAMA, Yoshiaki NAKAMURA

Aerodynamic Heating of a Gap in the Hypersonic Laminar Boundary

Trans. JSASS Aerospace Tech. Japan

Vol. 11, April 2013, pp.7-16

299.

Xiaopeng Xue, Hiroto KOYAMA, Yoshiaki NAKAMURA

Numerical Simulation of Supersonic Aerodynamic Interaction of a Parachute System


Vol. 11, May 2013, pp.33-42.

300.

奥津康彦, 濱本直樹、土井克則、中村佳朗

角柱近傍の平板が流れ場と音場に及ぼす影響

日本機械学会論文集（Ｂ編）、79巻、804号、August 2013、pp. 1397-1407.

301.

Yasuhiko OKUTSU, Naoki HAMAMOTO, Kazuo YANAGIMOTO, Katsunori DOI, Yoshiaki NAKAMURA

Verification of Automobile Aerodynamic Noise Transmitted through Side Window Glass

Journal of Environment and Engineering

Vol. 8, No.1, August 2013, pp.41-55.

302.

甲村圭司、中村佳朗

平板と楔による狭い隙間流れから発生する離散周波数騒音について


303.

甲村圭司、中村佳朗

シロッコファンにおける翼間流れの数値解析


304.

H. Yasuda, K. Kitamura, Yoshiaki NAKAMURA

Numerical Analysis of Flow Field and Aerodynamic Characteristics of a Quadrotor


Vol. 11, September 2013, pp.61-70.

- 37 -

305.

Xiaopeng XUE and Yoshiaki NAKAMURA

Numerical Simulation of a Three-Dimensional Flexible Parachute System under Supersonic

Conditions


Vol. 11, November 2013, pp.99-108.

306.

Shoya Mano, Keiichi Kitamura, Katsunori Doi and Yoshiaki Nakamura

Numerical Simulation Based on CFD for Aerodynamic Characteristics of Kite in Flight


Vol. 12, pp.1-10, February 2014

307.

Keiichi Ishiko, Atsushi Hashimoto, Yuichi Matsuo, Akira Yoshizawa, Yusuke Nishiyama, Koichi Mori and

Yoshiaki Nakaamura, One–Equation Extended Nonlinear Turbulence Modeling in Predicting Three-Dimensional Wall

Jets, Journal of Aircraft, March 2014, 51, 2, 2014, pp. 584-595.

[解説]

１．川添博光、中村佳朗

空力音発生における非圧縮性ジェット剪断層の役割

日本航空宇宙学会誌、第４３巻、第４９３号、1995, pp.75-81.

２．中村佳朗、石黒満津夫

ア－ク加熱風洞気流の電離特性について

日本航空宇宙学会誌、第４３巻、第４９９号、1995, pp. 467-472.

3. 中村佳朗、松野隆

後退角の大きくないデルタ翼のロール自励振動

日本航空宇宙学会誌、第４８巻、第５６０号、2000(９月)、pp. 490-494.

4. 中村佳朗

航空宇宙工学におけるこれからの流体力学

流体熱工学研究、第３７巻、第２号、2002(12月)、pp. 1-7.

5. 中村佳朗

航空宇宙工学におけるこれからのCFD

日本航空宇宙学会誌、第51巻、599号、2003、pp.300-305.

6. 中村佳朗

将来型航空機・宇宙機の空気力学に関する技術課題

機械の研究、56,1,1月号(2004), 51-57.

[著書]

１．数値流体力学東京大学出版会 (1992) 分担執筆

２．乱流の数値流体力学東京大学出版会（1998）分担執筆

- 38 -

３．流体実験ハンドブック朝倉書店（1997）分担執筆

４．計算力学ハンドブック（社)日本機械学会（2006）分担執筆

５．航空宇宙工学便覧丸善（2005）分担執筆

６．乱流工学ハンドブック朝倉書店(2009) pp.236-242 分担執筆

[監修]

１．ロケットエンジン(2003) 森北出版鈴木弘一著

２．ジェットエンジン（2004）森北出版鈴木弘一著