A review of the main problems in hypersonic aerothermodynamic and aerodynamic research is presented. To develop useful design tools for reentry vehicles, a balanced combination of computational fluid dynamics codes, wind tunnel experiments and free flight tests is needed. The designed facility is simple and cost effective, and is flown as piggyback in the second stage of Ariane 4.
Larve: A Hypersonic Flight-Test Facility Launched by Ariane 4
1989
6 pages
Report
Keine Angabe
Englisch
Second Ariane 5 Test Flight Successful
British Library Online Contents | 1997
NTIS | 1989
|AIAA | 1983
|Online Contents | 2001
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