Idealized Modeling and Analysis of the Shuttle Orbiter Wing Leading Edge Impact Data
AeroTech congress & exhibition ; 2007 ; Los Angeles, CA
01.01.2007
3882 pages
SAE 2007-01-3780 - 2007-01-3932 held with gaps
Aufsatz (Konferenz)
Englisch
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Idealized Modeling and Analysis of the Shuttle Orbiter Wing Leading Edge Impact Data
SAE Technical Papers | 2007
|Dynamic Impact Tolerance of Space Shuttle Orbiter Wing Leading-Edge Panels
Online Contents | 2008
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