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Flow structure generated by perpendicular blade-vortex interaction and implications for helicopter noise prediction.

著者名:
掲載資料名:
NASA Technical Reports
発行年:
1996
巻:
19960014827
号:
NASA-CR-200159
パート:
NAS 1.26:200159
ペーパー番号:
N96-21271
開始ページ:
1
出版情報:
National Aeronautics and Space Adminstration
言語:
英語
資料種別:
テクニカルペーパー

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