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
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