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