Preliminary Static Aeroelastic Analysis of Reusable Launch Vehicle Stability and Control Derivatives
Thomas A. Zeiler, David McGhee, Joseph A. Brunty
Journal of Spacecraft and Rockets ; 36 , 1 ; 67-74
1999-01-01
8 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
A Coupled Aeroelastic Model for Launch Vehicle Stability Analysis
British Library Conference Proceedings | 2010
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