AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL/VTOL - Finite Element Method Applied to Supersonic Flutter of Circular Cylindrical Shells
AIAA journal ; 48 , 1 ; 73-82
2010
Aufsatz (Zeitschrift)
Englisch
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL-VTOL - Damping Effects in Nonlinear Panel Flutter
Online Contents | 2000
|