A Computational Investigation of Flow Through an Axisymmetric Supersonic Inlet
48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
2010-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
A COMPUTATIONAL INVESTIGATION OF FLOW THROUGH AN AXISYMMETRIC SUPERSONIC INLET
British Library Conference Proceedings | 2010
|Axisymmetric nose inlet effects on supersonic airloads
AIAA | 1983
|Experimental Investigation of the Buzz Phenomenon in an Axisymmetric Supersonic Inlet
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