Application of Adjoint Methodology to Supersonic Aircraft Design Using Reversed Equivalent Areas
Author(s) -
Sriram K. Rallabhandi
Publication year - 2013
Publication title -
21st aiaa applied aerodynamics conference
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2013-2663
Subject(s) - supersonic speed , aerospace engineering , computer science , environmental science , engineering
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