Vortex-induced heating alleviation to lee side of slender wings in hypersonic flow by contouring leading edge planform
Alleviation of vortex-induced heating to the lee side of slender wings in hypersonic flow
1971-09-01
Sonstige
Keine Angabe
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
|