A study of a supersonic axisymmetric spiked inlet at angle of attackusing the Navier-Stokes equations
24th Aerospace Sciences Meeting ; 1986 ; Reno , NV , U.S.A.
01.01.1986
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Supersonic inlet study using the Navier-Stokes equations
AIAA | 1986
|Full Navier-Stokes Analysis of an Axisymmetric Scramjet Inlet
Online Contents | 1993
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