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An Approach to Constrained Aerodynamic Design With Application to Airfoils

著者名:
Campbell, Richard L ( Langley Research Center )  
掲載資料名:
NASA Technical Reports
発行年:
1992
号:
NASA-TP-3260
通号:
H1/02 0128403
パート:
NAS 1.60:3260
ペーパー番号:
N93-12321
開始ページ:
1
終了ページ:
24
総ページ数:
24
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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