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ArticleJ-GLOBAL ID:200902001948432534整理番号:85A0414390

Scaling of airfoil self-noise using measured flow parameters.

測定した流れのパラメータを用いる翼型自己騒音の寸法効果

著者:BROOKS T F(NASA Langley Research Center, Virginia)、MARCOLINI M A(NASA Langley Research Center, Virginia)
資料名:AIAA J (Am Inst Aeronaut Astronaut) 巻:23 号:2 ページ:207-213
発行年:1985年02月
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