Transition Measurement Using Hot-Film on Supersonic Experimental Airplane NEXST-1
2007
71 pages
Report
No indication
English
Transition Measurement of Natural Laminar Flow Wing on Supersonic Experimental Airplane NEXST-1
Online Contents | 2008
|Static Aeroelastic Analysis of Supersonic Experimental Airplane NEXST-1 Flight Test
British Library Conference Proceedings | 2007
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