PITCH - FLAP FLUTTER INSTABILITY OF COMPOSITE ROTORCRAFT BLADE WITH NON-UNIFORM CROSS SECTION IN UNSTEADY SUBSONIC COMPRESSIBLE FLOW
International annual forum; 69th, American Helicopter Society; Vertical Flight Technical Society ; 2013 ; Phoenix, AZ
2013-01-01
15 pages
Includes bibliographical references and index
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Flutter Stability of a Detuned Cascade in Subsonic Compressible Flow
British Library Conference Proceedings | 1994
|Flutter Stability of a Detuned Cascade in Subsonic Compressible Flow
Online Contents | 1995
|