| タイトル | CFD Results for an Axisymmetric Isentropic Relaxed Compression Inlet |
| 本文（外部サイト） | http://hdl.handle.net/2060/20090002599 |
| 著者（英） | Conners, Timothy R.; Tacina, Kathleen M.; Hirt, Stefanie M.; Merret, Jason M.; Howe, Donald C. |
| 著者所属（英） | NASA Glenn Research Center |
| 発行日 | 2008-11-01 |
| 言語 | eng |
| 内容記述 | The OVERFLOW code was used to calculate the flow field for a family of five relaxed compression inlets, which were part of a screening study to determine a configuration most suited to the application of microscale flow control technology as a replacement for bleed. Comparisons are made to experimental data collected for each of the inlets in the 1- by 1-Foot Supersonic Wind Tunnel at the NASA Glenn Research Center (GRC) to help determine the suitability of computational fluid dynamics (CFD) as a tool for future studies of these inlets with flow control devices. Effects on the wind tunnel results of the struts present in a high subsonic flow region accounted for most of the inconsistency between the results. Based on the level of agreement in the present study, it is expected that CFD can be used as a tool to aid in the design of a study of this class of inlets with flow control. |
| NASA分類 | Aerodynamics |
| レポートNO | E-16580
AIAA Paper-2008-0092
NASA/TM-2008-215416 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/254538 |
