An airflow at 25-degrees C and 50 kPa with a velocity of 900 m/s is turned by an abrupt 25-degree corner with a weak oblique shock. Estimate the pressure (in kPa), velocity (in m/s), and Mach number after the corner. 110 kPa, 540 m/s, 1.38 124 kPa, 602 m/s, 1.51 144 kPa. 668 m/s, 1.72 162 kPa, 689 m/s. 1.80 None of the above

An airflow at 25-degrees C and 50 kPa with a velocity of 900 m/s is turned by an abrupt 25-degree corner with a weak oblique shock. Estimate the pressure (in kPa), velocity (in m/s), and Mach number after the corner. 110 kPa, 540 m/s, 1.38 124 kPa, 602 m/s, 1.51 144 kPa. 668 m/s, 1.72 162 kPa, 689 m/s. 1.80 None of the above

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

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