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
Article (Journal)
Electronic Resource
English
Aerodynamic Wing Design of NEXST-2 Using Unstructured-Mesh and Supersonic Inverse Problem
Online Contents | 2004
|Transition Measurement of Natural Laminar Flow Wing on Supersonic Experimental Airplane NEXST-1
Online Contents | 2008
|