Characteristics of Turbulent Boundary Layers along a Hypersonic Vehicle
<p> The flight conditions of a hypersonic vehicle on an ascent trajectory are computed and Reynolds-averaged Navier-Stokes (RANS) simulations of the turbulent boundary layers are performed across a Mach number range of 0.3 up to 16 using the computational fluid dynamics (CFD) software, VULCAN....
| Main Author: | |
|---|---|
| Language: | EN |
| Published: |
State University of New York at Buffalo
2018
|
| Subjects: | |
| Online Access: | http://pqdtopen.proquest.com/#viewpdf?dispub=10822170 |