![](/img/cover-not-exists.png)
Application of Adjoint Methodology to Supersonic Aircraft Design Using Reversed Equivalent Areas
Rallabhandi, Sriram K.Volume:
51
Language:
english
Journal:
Journal of Aircraft
DOI:
10.2514/1.C032518
Date:
November, 2014
File:
PDF, 5.50 MB
english, 2014