2 Calculate the mass flow and the annulus area at the rotor outlet for an...
90.2K
Verified Solution
Link Copied!
Question
Basic Math
2 Calculate the mass flow and the annulus area at the rotor outlet for an axial compressor stage The flow enters the rotor without swirl at a Mach number of 0 4 at a stagnation pressure of 200 kPa and a stagnation temperature of 370 K in an annulus of area 0 17 m The axial velocity is constant across the rotor but the flow leaves at 30 6 degrees to the axial direction The stagnation pressure at the rotor outlet is 230 kPa and the stagnation to stagnation polytropic efficiency to this point is 0 94 Use properties of air as k 1 4and Cp 1008 9 J Kg K
Answer & Explanation
Solved by verified expert
Get Answers to Unlimited Questions
Join us to gain access to millions of questions and expert answers. Enjoy exclusive benefits tailored just for you!
Membership Benefits:
Unlimited Question Access with detailed Answers
Zin AI - 3 Million Words
10 Dall-E 3 Images
20 Plot Generations
Conversation with Dialogue Memory
No Ads, Ever!
Access to Our Best AI Platform: Zin AI - Your personal assistant for all your inquiries!
