| タイトル | Flight experiments studying the growth of the disturbances in the laminar boundary layer |
| 著者（英） | Wusk, Michael S.; Lee, Cynthia C.; Obara, Clifford J. |
| 著者所属（英） | Lockheed Engineering and Sciences Co.; NASA Langley Research Center; Analytical Services and Materials, Inc. |
| 発行日 | 1990-10-01 |
| 言語 | eng |
| 内容記述 | Results are presented from flight experiments conducted on a gloved aircraft wing surface, incorporating closely-spaced flush-mounted and streamwise-located instrumentation for instability frequencies and pressure distributions, which studied the growth of disturbances in the laminar boundary layer. Mach numbers up to 0.81 were encountered in order to obtain compressible-condition measurements; this exploration therefore encompassed chord Reynolds number conditions of the order of 10-20 million, as well as the introduction of sweep via sideslip maneuvers, and the effects of cloud particles. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 91A48641
SAE PAPER 901979 |
| 権利 | Copyright |
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