Alleviation of vortex-induced heating to the lee side of slender wings in hypersonic flow
BERTRAM, M. H. /NASA, LANGLEY RESEARCH CENTER, HAMPTON, VA./., WHITEHEAD, A. H., JR.
AIAA Journal ; 9 , 9 ; 1870-1872
1971-01-01
3 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Sulsonic vortex-flow desig study for slender wings
Tema Archiv | 1978
|Subsonic Vortex-Flow Design Study for Slender Wings
AIAA | 1978
|Subsonic vortex-flow design study for slender wings
Tema Archiv | 1978
|Subsonic vortex-flow design study for slender wings
AIAA | 1978
|