Numerical and Experimental Tests of a Supersonic Inlet Utilizing a Pylon Set for Mixing, Combustion and Thrust Enhancement
43rd:; meeting.; MEETING AND EXHIBIT, Aerospace sciences ; 2005 ; Reno, NV
01.01.2005
AIAA 2005-21
2005-0019 - 2005-1421 with gaps
Aufsatz (Konferenz)
Englisch
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Experimental study of mixing enhancement using pylon in supersonic flow
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