Q7- Air flowing with a Mach number of 2 with a pressure of 80 kPa and a temperatureof 30 °C passes over a component of an aircraft that can be modeled as a wedge with anincluded angle of 8° that is aligned with the flow, the flow is turned through an angle of4 leading to the generation of an oblique shock wave. Find the pressure acting on thesurface of the wedge.M 2P = 80 kPaT = 30°C

Data given M1 =2P1 =80 KPaT1 =30° c =303° Kflows turning angle θ= 4° from θ-β-M relation…

Answered: KP s over a component of an aircraft…

KP s over a component of an aircraft that can be modeled of 8° that is aligned with the flow, the flow is turned the generation of an oblique shock wave. Find the pre vedge.

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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Question

Q7- Air flowing with a Mach number of 2 with a pressure of 80 kPa and a temperature
of 30 °C passes over a component of an aircraft that can be modeled as a wedge with an
included angle of 8° that is aligned with the flow, the flow is turned through an angle of
4 leading to the generation of an oblique shock wave. Find the pressure acting on the
surface of the wedge.
M 2
P = 80 kPa
T = 30°C

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