NUMERICAL PREDICTION OF STAGNATION-POINT SHOCK-DETACHMENT DISTANCE FOR HYPERSONIC LOW DENSITY FLOW OVER BLUNT NOSE SHAPES
24th, International congresss of aeronautical sciences ; 2004 ; Yokohama, Japan
01.01.2004
ICAS 2004-3.7.R.1
Also known as ICAS 2004.; HELD ON CD-ROM
Aufsatz (Konferenz)
Englisch
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