| タイトル | Upper wing surface boundary layer measurements and static aerodynamic data obtained on a 0.015-scale model (42-0) or the SSV orbiter configuration 140A/B in the LTV HSWT at a Mach number of 4.6 (LA58) |
| 本文（外部サイト） | http://hdl.handle.net/2060/19760011131 |
| 著者（英） | Ball, J. W.; Lindahl, R. H. |
| 著者所属（英） | Chrysler Corp. |
| 発行日 | 1976-02-01 |
| 言語 | eng |
| 内容記述 | The purpose of the test was to investigate the nature of the Orbiter boundary layer characteristics at angles of attack from -4 to 32 degrees at a Mach number of 4.6. The effect of large grit, employed as transition strips, on both the nature of the boundary layer and the force and moment characteristics were investigated along with the effects of large negative elevon deflection on lee side separation. In addition, laminar and turbulent boundary layer separation phenomena which could cause asymmetric flow separation were investigated. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 76N18219
DMS-DR-2215
NASA-CR-144592 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/186959 |
