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Boundary layer transition analysis on NEXST-1 airplane: NAL-ONERA cooperative research project
Boundary layer transition analysis on NEXST-1 airplane: NAL-ONERA cooperative research project
2007
Kenji Yoshida
Yoshine Ueda
Hiroki Sugiura
Naoko Tokugawa
Takashi Atobe
Daniel Arnal
Jean-Pierre Archambaud
Alain Seraudie
yosida kenzi
ueda ryou ine
sugiura hiroki
tokugawa naoko
atobe takasi
Keywords:
Airplane
Aeronautics
Supersonic wind tunnel
Computational fluid dynamics
Boundary layer
Physics
Aerospace engineering
cooperative research
Marine engineering
Geology
wind tunnel test
Choked flow
Correction
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