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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Transcribed Image Text: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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