Que: Air flowing at Machn 2.5 with a pressure of 60 kPa and a temperature of 2020°C passes over a wedge which turns the flow through an angle of 44leading to the generation of oblique shock waves One of the oblique shock waves impinges on a flat wall, which is parallel to the flow upstream of the wedge and is " from it Find the pressure and velocity behind the reflected shock wave GIVE MATLAB CODE TO SOLVE ?

Que: Air flowing at Machn 2.5 with a pressure of 60 kPa and a temperature of 2020°C passes over a wedge which turns the flow through an angle of 44leading to the generation of oblique shock waves One of the oblique shock waves impinges on a flat wall, which is parallel to the flow upstream of the wedge and is " from it Find the pressure and velocity behind the reflected shock wave GIVE MATLAB CODE TO SOLVE ?

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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Question

write MATLAB scripts to solve the following. Give MATLAB CODE :
Que: Air flowing at Mach 2.5 with a pressure of 60 kPa and a temperature
of 2020°C passes over
a wedge which turns the flow through an angle of 44 leading to the
generation of oblique shock
waves One of the oblique shock waves impinges on a flat wall, which is
parallel to the flow
upstream of the wedge and is. " from it Find the pressure and velocity
behind the
reflected shock wave
GIVE MATLAB CODE TO SOLVE ?

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