Application of Adjoint Methodology to Supersonic Aircraft...

Application of Adjoint Methodology to Supersonic Aircraft Design Using Reversed Equivalent Areas

Rallabhandi, Sriram K.
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Volume:
51
Language:
english
Journal:
Journal of Aircraft
DOI:
10.2514/1.C032518
Date:
November, 2014
File:
PDF, 5.50 MB
english, 2014
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