| タイトル | OVERFLOW Simulations of Space Shuttle Orbiter Reentry Based on As-Built Geometry |
| 本文（外部サイト） | http://hdl.handle.net/2060/20120017918 |
| 著者（英） | Vicker, Darby J.; Wilson, Brad; Ma, Edward C.; Pavek, Mike; Berger, Karen; Campbell, Charles H. |
| 著者所属（英） | NASA Johnson Space Center |
| 発行日 | 2012-06-24 |
| 言語 | eng |
| 内容記述 | The Space Shuttle Orbiters Discovery and Endeavor have been digitally scanned to obtain outer mold line surfaces. Using these scans, the existing overset computational fluid dynamics (CFD) grid system will be modified by projecting the grid points to the scanned geometry. Simulations will be performed using the OVERFLOW solver and the results compared to previous OVERFLOW results on the theoretical geometry and the aerodynamic databook. The "bent airframe" term will be compared between the aerodynamic databook and the computations over a range of reentry conditions. |
| NASA分類 | Spacecraft Design, Testing and Performance |
| レポートNO | JSC-CN-27558 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
