AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL-VTOL - Effect of Airfoil Aerodynamic Loading on Trailing-Edge Noise Sources
AIAA journal ; 43 , 1 ; 41-52
2005
Aufsatz (Zeitschrift)
Englisch
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL-VTOL - Trailing-Edge Flap Control of Dynamic Pitching Moment
Online Contents | 2007
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