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ArticleJ-GLOBAL ID:200902015494147504整理番号:89A0111629

Wing laminar boundary layer in the presence of a propeller slipstream.

プロペラ滑り流がある場合の翼の層流境界層

著者:MILEY S J(Texas A&M Univ., TX, USA)、HOWARD R M(Texas A&M Univ., TX, USA)、HOLMES B J(NASA Langley Research Center, VA, USA)
資料名:Congr Int Counc Aeronaut Sci 巻:15th 号:2 ページ:1413-1420
発行年:1986年
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