Analyses of Foam Impact onto the Columbia Shuttle Wing Leading Edge Panels Using Pronto3d/SPH
42nd AIAA Aerospace Sciences Meeting and Exhibit
01.01.2004
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
ANALYSES OF FOAM IMPACT ONTO THE COLUMBIA SHUTTLE WING LEADING EDGE PANELS USING PRONTO3D/SPH
British Library Conference Proceedings | 2004
|Dynamic Impact Tolerance of Space Shuttle Orbiter Wing Leading-Edge Panels
Online Contents | 2008
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