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rotor blade mean radius = (rtip + Thub) / 2 Thub Itip hub to tip radius ratio Angles α1, B1, α2, ẞ2 are: = 20 cm = 0.8 Cz1 Cz2 axial velocity = 40°, 60°, 60°, 40° respectively = 125 m/s static pressure, temperature p₁, T₁ upstream of rotor = 0.5 atm. and 20° C respectively stage efficiency nst = 0.90

rotor blade mean radius = (rtip + Thub) / 2 Thub Itip hub to tip radius ratio Angles α1, B1, α2, ẞ2 are: = 20 cm = 0.8 Cz1 Cz2 axial velocity = 40°, 60°, 60°, 40° respectively = 125 m/s static pressure, temperature p₁, T₁ upstream of rotor = 0.5 atm. and 20° C respectively stage efficiency nst = 0.90

Introductory Circuit Analysis (13th Edition)
Introductory Circuit Analysis (13th Edition)
13th Edition
ISBN:9780133923605
Author:Robert L. Boylestad
Publisher:Robert L. Boylestad
Chapter1: Introduction
Section: Chapter Questions
Problem 1P: Visit your local library (at school or home) and describe the extent to which it provides literature...
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Please help me by giving an answer for this, also I need help with using this question, and bartleby assign this to a mechanical engineer please.
One stage of an axial compressor has the following properties:
a) What is the shaft RPM (N) in revolutions per minute ?
b) What is the mass flow rate in kg/s ?
c) What is the power required to operate this stage, in kWatts ?
 
 
rotor blade mean radius = (rtip + Thub) / 2 Thub Itip hub to tip radius ratio Angles α1, B1, α2, ẞ2 are: = 20 cm = 0.8 Cz1 Cz2 axial velocity = 40°, 60°, 60°, 40° respectively = 125 m/s static pressure, temperature p₁, T₁ upstream of rotor = 0.5 atm. and 20° C respectively stage efficiency nst = 0.90
Transcribed Image Text:rotor blade mean radius = (rtip + Thub) / 2 Thub Itip hub to tip radius ratio Angles α1, B1, α2, ẞ2 are: = 20 cm = 0.8 Cz1 Cz2 axial velocity = 40°, 60°, 60°, 40° respectively = 125 m/s static pressure, temperature p₁, T₁ upstream of rotor = 0.5 atm. and 20° C respectively stage efficiency nst = 0.90
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