Aerodynamic Wing Design of NEXST-2 Using Unstructured-Mesh and Supersonic Inverse Problem

An efficient aerodynamic design system is developed and applied to design natural laminar flow wings of the experimental supersonic airplanes of the National Aerospace Laboratory (NAL) in Japan. In the design system developed, an inverse problem solver using integral equations is employed in the des...

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Veröffentlicht in:	Journal of aircraft 2004-09, Vol.41 (5), p.1146-1152
Hauptverfasser:	Fujita, Takeshi, Matsushima, Kisa, Nakahashi, Kazuhiro
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Air transportation and traffic Aircraft Applied sciences Design Exact sciences and technology Fluid dynamics Ground, air and sea transportation, marine construction
Online-Zugang:	Volltext
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