Transitional Shock Wave-Boundary Layer Interaction over a Cone Flare Model at Hypersonic Conditions
European symposium; 4th, Aerothermodynamics for space vehicles ; 2001 ; Capua, Italy
01.01.2002
8 pages
One CD-ROM in pocket attached to inside back cover
Aufsatz (Konferenz)
Englisch
space vehicles , ASI , ESA , aerothermodynamics , CIRA
© Metadata Copyright the British Library Board and other contributors. All rights reserved.