Elastic deflection effects on transonic aerodynamics of a flutter wing model with control surfaces-Reference-Cited by-同舟云学术

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Elastic deflection effects on transonic aerodynamics of a flutter wing model with control surfaces

Published:1995-08-22 Issue: Volume: Page:
ISSN:
Container-title:Aircraft Engineering, Technology, and Operations Congress
language:
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Author:

Saitoh K,Hashidate M,Matsushita H,Kikuchi T

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1995-3926

Reference15 articles.

1. Role of Shocks in the "Sub-Transonic" Flutter Phenomenon

2. ZDowell,E. H. "Nonlinear Aeroelasticity," Chapter 4, Val.5:StructuralDynamicsandAeroelasticity, Noor,A. K. andVenneri,S.L.,ed.,ASME,1993,pp.213-239.

3. 3Mabey,D. G. "Physical PhenomenaAssociated with UnsteadyTransonicFlows,"Chapter 1,Unsteady Transonic Aerodynamics, A M , 1989,pp. 1-55.

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