Laminar, transition, and turbulent boundary- layer characteristic with favorable pressure gradient M sub 1 equals 9.6
NAGAMATSU, H. T., SHEER, R. E., JR. /GE RESEARCH AND DEVELOPMENT CENTER, SCHENECTADY, N.Y./., WISLER, D. C.
Journal of Aircraft ; 8 , 3 ; 176-182
1971
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 2006
|