Parameters contributing to aeroelastic problems in thermal protection of space shuttle
Application of recent panel flutter research to the space shuttle. Part 2 - Influence of edge clips and flow angularity
1971-04-01
Sonstige
Keine Angabe
Englisch
Effects of Flow Angularity on Nonlinear Supersonic Flutter of Composite Panels
British Library Conference Proceedings | 1999
|Flutter technology for space shuttle
NTRS | 1972
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