Boundary-layer transition measurements on swept wings with supersonic leading edges.
GROTH, E. E. /NORTHROP CORP., NORAIR DIV., HAWTHORNE, CALIF./., PATE,S. R. /ARO, INC., ARNOLD ENGINEERING DEVELOPMENT CENTER, VON KARMAN GAS DYNAMICS FACILITY, SUPE
AIAA Journal ; 4 , 4 ; 737-738
1966
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Optimum supersonic wings with subsonic leading edges
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