AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL-VTOL - Nonlinear Aeroelastic Computations of a Wing-Pylon-Finned-Store Using Parallel Computing
AIAA journal ; 43 , 1 ; 53-62
2005
Aufsatz (Zeitschrift)
Englisch
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL Nonlinear Aeroelastic Study for Folding Wing Structures
Online Contents | 2010
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