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
2004-01-01
ICAS 2004-3.7.R.1
Also known as ICAS 2004.; HELD ON CD-ROM
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.