JAXA Special Publication: Proceedings of the 33rd and 34th JAXA Workshops on Investigation and Control of Boundary-Layer Transition
巻
JAXA-SP-04-002
ページ
33 - 34
発行年
2005-01-28
抄録（英）
Experimental investigation of the boundary-layer transition on a 10-deg sharp cone at 2-deg incidence was conducted at Mach 2. Transition locations were obtained with small surface roughness on the order of 0.1 micron using an infrared camera. The result showed that the most forward transition occurred on the side rather than on the leeward ray as observed in the previous studies. The comparison of the transition front was made between two supersonic tunnels with similar turbulence levels.
迎角を有する円錐の超音速3次元境界層の遷移計測
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