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Robust airfoil optimization to achieve drag reduction over a range of Mach numbers
Robust airfoil optimization to achieve drag reduction over a range of Mach numbers
Robust airfoil optimization to achieve drag reduction over a range of Mach numbers
Li, W. (Autor:in) / Huyse, L. (Autor:in) / Padula, S. (Autor:in)
STRUCTURAL AND MULTIDISCIPLINARY OPTIMIZATION ; 24 ; 38-50
01.01.2002
13 pages
Aufsatz (Zeitschrift)
Englisch
DDC:
624.17713
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