Course Project for High Speed Aerodynamics (AAE 4083) at the Manipal Institute of Technology, Manipal, India

Problem Statement

Simulate the flow over a wedge and a blunt body flying at an altitude of 25 km and at Mach 9.

Mesh

Mesh of the Wedge
Mesh of the Wedge
Mesh of the Blunt Body
Mesh of the Blunt Body


Pressure Distribution

Pressure Distribution Around the Wedge
Pressure Distribution about the Wedge
Pressure Distribution Around the Blunt Body
Pressure Distribution about the Blunt Body


Temperature Distribution

Image 1
Static Temperature Distribution about the Wedge
Image 2
Static Temperature Distribution about the Blunt Body


Density Variation

Image 1
Density Variation about the Wedge
Image 2
Density Varation about the Blunt Body


Velocity Distribution

Image 1
Velocity Distribution about the Wedge
Image 2
Velocity Distribution About the Blunt Body