ca 3 407

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Registration No.:____ _____________ Set A Te st-3 Course: MEC407::TURBOMACHNER!  Se"tion M#E$0 Ti%e A&&o'e(: )0 %inutes Ma*. Mar+s: 30 A&& ,uestions are "o%u&sor. /  Briefly explain the following (a) Sur gin g an d Choki ng. 1) %ar+s2 (b) Input and Output ve locity tr iangles f or backward and radial blades  1) %ar+s2 / # iscuss all the perfor!ance para!eters for centrifugal co!pressor in detail and also explain the effect of these on the perfor!ance of co!pressor . 10 %ar+s2 / 3 " centrifuga l co!pressor co!presses #$ kg%s of air at &'$$$ rp!. he air enters the co!pressor axially and the conditions at the exit sections are radius * $.#! relative velocity of air at tip * &$$!%s at an angle of +$ $  with respect to plane of rotation. ake p $& * & bar and $& * #$$,. -ind the torue and power reuired to drive the co!pressor and also the head developed. 10 %ar+s2 Registration No.:____ _____________ Set A Test-3 Course: MEC407::TURBOMACHNER! Se"tion M#E$0 Ti%e A&&o'e(: )0 %inutes Ma*. Mar+s: 30 A&& ,uestions are "o%u&sor. /  Briefly explain the following (a) Sur gin g an d Choki ng. 1) %ar+s2 (b) Input and Output ve locity tr iangles f or backward and radi al blades  1) %ar+s2 / # iscuss all the perfor!ance para!eters for centrifugal co!pressor in detail and also explain the effect of these on the perfor!ance of co!pressor . 10 %ar+s2 / 3 " centrifuga l co!pressor co!presses #$ kg%s of air at &'$$$ rp!. he air enters the co!pressor axially and the conditions at the exit sections are radius * $.#! relative velocity of air at tip * &$$!%s at an angle of +$ $  with respect to plane of rotation. ake p $& * & bar and $& * #$$,. -ind the torue and power reuired to drive the

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7/23/2019 CA 3 407

http://slidepdf.com/reader/full/ca-3-407 1/2

Registration No.:_________________ Set A Test-3

Course: MEC407::TURBOMACHNER!

 Se"tion M#E$0 Ti%e A&&o'e(: )0 %inutes Ma*. Mar+s: 30

A&& ,uestions are "o%u&sor.

/  Briefly explain the following

(a) Surging and Choking. 1) %ar+s2 (b) Input and Output velocity triangles for backward and radial blades  1) %ar+s2

/ # iscuss all the perfor!ance para!eters for centrifugal co!pressor in detail and also explain the effect of these

on the perfor!ance of co!pressor. 10 %ar+s2

/ 3 " centrifugal co!pressor co!presses #$ kg%s of air at &'$$$ rp!. he air enters the co!pressor axially and the

conditions at the exit sections are radius * $.#! relative velocity of air at tip * &$$!%s at an angle of +$ $ with

respect to plane of rotation. ake p $& * & bar and $& * #$$,. -ind the torue and power reuired to drive the

co!pressor and also the head developed.

10 %ar+s2

Registration No.:_________________ Set A Test-3

Course: MEC407::TURBOMACHNER!

 Se"tion M#E$0 Ti%e A&&o'e(: )0 %inutes Ma*. Mar+s: 30

A&& ,uestions are "o%u&sor.

/  Briefly explain the following

(a) Surging and Choking. 1) %ar+s2 

(b) Input and Output velocity triangles for backward and radial blades  1) %ar+s2

/ # iscuss all the perfor!ance para!eters for centrifugal co!pressor in detail and also explain the effect of these

on the perfor!ance of co!pressor. 10 %ar+s2

/ 3 " centrifugal co!pressor co!presses #$ kg%s of air at &'$$$ rp!. he air enters the co!pressor axially and the

conditions at the exit sections are radius * $.#! relative velocity of air at tip * &$$!%s at an angle of +$ $ with

respect to plane of rotation. ake p $& * & bar and $& * #$$,. -ind the torue and power reuired to drive the

7/23/2019 CA 3 407

http://slidepdf.com/reader/full/ca-3-407 2/2

co!pressor and also the head developed.

10 %ar+s2