AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL-VTOL - Nonlinear Flutter Calculations Using Finite Elements in a Direct Eulerian-Lagrangian Formulation
AIAA journal ; 46 , 6 ; 1331-1341
2008
Aufsatz (Zeitschrift)
Englisch
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL-VTOL - Damping Effects in Nonlinear Panel Flutter
Online Contents | 2000
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