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ArticleJ-GLOBAL ID:200902076590080550整理番号:82A0175513

Crossflow effects on steady and fluctuating pressures on an ogive-cylinder cone-frustum model in supersonic separated flow.

超音速はく離流中のオジャイブ‐円柱‐円すい‐円すい台模型上の定常および変動圧力におよぼす横断流効果

著者:DODS J B JR(Raman Aeronautics, Inc., California)、COE C F(Ames Research Center, California)
資料名:NASA Tech Pap ページ:60P
発行年:1981年11月
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