AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL-VTOL - Novel Boundary Integral Formulation for Blade-Vortex Interaction Aerodynamics of Helicopter Rotors
AIAA journal ; 45 , 6 ; 1169-1176
2007
Aufsatz (Zeitschrift)
Englisch
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL-VTOL - Transonic Helicopter Noise
Online Contents | 2005
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