choose the correct answers 12:07ll ?A alfarahidiuc.comAnswer all of the questionQ2/ In an axial flow compressor, airenters at a stagnation temperature of290 K and 1 bar. The axial velocity ofair is 180 m/s (constant throughout thestage), the absolute velocity at theinlet is 185 m/s, the work done factoris 0.86 , and the degree of reaction is50%. If the stage efficiency is 0.86,calculate the air angles at the rotorinlet and outlet and the stagnationtemperature rise of the stage andstage pressure ratio. Assume a rotorspeed of 200 m/s. hint : Cp = 1005J/kg.k and X = 1.4 a) a1=B2=13.350 ,a2=B1=41.150 , ATos = 19.62 K , nstage= 1.22 b) a1=B2=15.250 , a2=B1=38.260ATos = 16.24K , nstage = 1.45 c)a1=B2=16.780 , a2=B1=47.780 , ATos =13.64 K, Tnstage = 1.35 d)a1=B2=18.350 , a2=B1=35.160 , ATos =19.62 K , nstage = 1.89 e) None of%3D%3D%3DaboveO aObOcOdOeارسال الاجابةخروجعد د الاسئلة :701:22:24

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Answered: Q2/ In an axial flow compresse

Engineering

Mechanical Engineering

Q2/ In an axial flow compresse

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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