AEROELASTIC ANALYSIS OF AN SST TYPED WING WITH A TRAILING EDGE FLAP USING A CHIMERA GRID APPROACH
42nd:; Meeting, Aerospace sciences ; 2004 ; Reno, NV
01.01.2004
AIAA 2004-1271
AIAA 2004-0001 - AIAA 2004-1388 held with gaps
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
British Library Conference Proceedings | 2015
|Aeroelastic Stability of Trailing-Edge Flap Helicopter Rotors
Online Contents | 2003
|SAE Technical Papers | 2015
|