AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL-VTOL - Aeroelastic Response of Nonlinear Wing Sections Using a Functional Series Technique
AIAA journal ; 40 , 5 ; 813-823
2002
Aufsatz (Zeitschrift)
Englisch
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL Nonlinear Aeroelastic Study for Folding Wing Structures
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