AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL-VTOL - Freestream Pulsation Effects on the Aeroelastic Response of a Finite Wing
AIAA journal ; 46 , 11 ; 2723-2729
2008
Aufsatz (Zeitschrift)
Englisch
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL Nonlinear Aeroelastic Study for Folding Wing Structures
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