Wind Tunnel Tests and Analysis on Flutter of Spacecraft Including Pitching Effects in Its Launching Configuration
International forum, Aeroelasticity and structural dynamics: CEAS/AIAA/ICASE/NASA Langley international forum on aeroelasticity and structural dynamics 1999 ; 1999 ; Williamsburg; VA
Aeroelasticity and structural dynamics: CEAS/AIAA/ICASE/NASA Langley international forum on aeroelasticity and structural dynamics 1999 ; 209136 ; 115-120
NASA CONFERENCE PUBLICATION ; 209136
1999-01-01
6 pages
Aufsatz (Konferenz)
Englisch
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Wind-Tunnel Tests for Active Flutter Control and Closed-Loop Flutter Identification
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