Wind Tunnel Tests for Separation Dynamics Modeling of a Two-Stage Hypersonic Vehicle
International conference; 10th, Space planes and hypersonic systems and technologies ; 2001 ; Kyoto, Japan
2001-01-01
10 pages
Contains papers AIAA-2001-1750 to 1927 only with gaps
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.