Magazine Article

Space Propulsion Design and Analysis

TBMG-2359

09/01/2007

Abstract
Content

This software provides an improved methodology for predicting launcher base pressure and heat loads for RSRM (Reusable Solid Rocket Motor) launchers by accounting for complex anisotropic stress/ strains and variable turbulent Prandtl and Schmidt numbers. A “building block” approach to turbulence model development, and validation has been applied for improved missile/ launcher base region analysis.

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Citation
"Space Propulsion Design and Analysis," Mobility Engineering, September 1, 2007.
Additional Details
Publisher
Published
Sep 1, 2007
Product Code
TBMG-2359
Content Type
Magazine Article
Language
English