| タイトル | Heat Transfer from a Hemisphere-cylinder Equipped with Flow-separation Spikes |
| 本文（外部サイト） | http://hdl.handle.net/2060/19930083996 |
| 著者（英） | Nielsen, Helmer V; Stalder, Jackson R |
| 著者所属（英） | National Advisory Committee for Aeronautics. Ames Aeronautical Lab. |
| 発行日 | 1954-09-01 |
| 言語 | eng |
| 内容記述 | Average heat-transfer, temperature-recovery, and pressure-distribution measurements were obtained over the hemispherical nose of a body of revolution both with and without flow-separation spikes. The tests, conducted in a range of Reynolds numbers from 1.55 to 9.85 x 10(5) and from Mach number 0.12 to 5.04, indicated that in supersonic flow the addition of spikes approximately doubles the rate of heat transfer, regardless of spike length. |
| レポートNO | 93R13286
NACA-TN-3287 |
| 権利 | No Copyright |
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