Space Propulsion Design and Analysis
TBMG-2359
09/01/2007
- 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.
- Citation
- "Space Propulsion Design and Analysis," Mobility Engineering, September 1, 2007.