Transition Measurement of Natural Laminar Flow Wing on Supersonic Experimental Airplane NEXST-1
Journal of Aircraft ; 45 , 5 ; 1495-1504
01.09.2008
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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