ICAS2014_0423: AEROELASTIC PREDICTION FOR MISSILE FINS IN SUPERSONIC FLOWS
International Council of the Aeronautical Sciences (Congress)
2014-01-01
10 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Aeroelastic/Aeroservoelastic Tailoring for Hinge Moment Minimization of Missile Fins
British Library Conference Proceedings | 1998
|Grid fins for missile applications in supersonic flow
AIAA | 1996
|Effect of thickness and angle-of-attack on the aeroelastic stability of supersonic fins
Online Contents | 2012
|Aeroelastic Optimization of Sounding Rocket Fins
NTIS | 2009
|