Aerodynamic Wing Design of NEXST-2 Using Unstructured-Mesh and Supersonic Inverse Problem
Takeshi Fujita, Kisa Matsushima, Kazuhiro Nakahashi
Journal of Aircraft ; 41 , 5 ; 1146-1152
2004-01-01
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Aerodynamic Wing Design of NEXST-2 Using Unstructured-Mesh and Supersonic Inverse Problem
Online Contents | 2004
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