AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL Nonlinear Aeroelastic Study for Folding Wing Structures
AIAA journal ; 48 , 10 ; 2187-2196
2010
Aufsatz (Zeitschrift)
Englisch
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Aeroelastic-Acoustics Simulation of Flight Systems
Online Contents | 2010
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