QUESTION 1 Inlet stagnation air pressure of a two-dimensional compressor cascade is 1.0 bar and inlet stagnation temperature of 295K. For an inlet Mach number of 0.75 and an inlet flow angle of 480, the exit flow angle is measured as 16.50. Assuming the flow is isentropic, determine the mass flow rate per unit frontal area, the exit Mach number and the static pressure ratio across the cascade

QUESTION 1 Inlet stagnation air pressure of a two-dimensional compressor cascade is 1.0 bar and inlet stagnation temperature of 295K. For an inlet Mach number of 0.75 and an inlet flow angle of 480, the exit flow angle is measured as 16.50. Assuming the flow is isentropic, determine the mass flow rate per unit frontal area, the exit Mach number and the static pressure ratio across the cascade

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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