| タイトル | Comparison of Theoretical and Experimental Heat-Transfer Characteristics of Bodies of Revolution at Supersonic Speeds |
| 本文（外部サイト） | http://hdl.handle.net/2060/19930092100 |
| 著者（英） | Scherrer, Richard |
| 著者所属（英） | National Advisory Committee for Aeronautics. Ames Aeronautical Lab. |
| 発行日 | 1951-01-01 |
| 言語 | eng |
| 内容記述 | An investigation of the three important factors that determine convective heat-transfer characteristics at supersonic speeds, location boundary-layer transition, recovery factor, and heat-transfer parameter has been performed at Mach numbers from 1.49 to 1.18. The bodies of revolution that were tested had, in most cases, laminar boundary layers, and the test results have been compared with available theory. Boundary-layer transition was found to be affected by heat transfer. Adding heat to a laminar boundary layer caused transition to move forward on the test body, while removing heat caused transition to move rearward. These experimental results and the implications of boundary-layer-stability theory are in qualitative agreement. |
| レポートNO | 93R21390
NACA-TR-1055 |
| 権利 | No Copyright |
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