Limited amplitude panel flutter with a temperature differential-Reference-Cited by-同舟云学术

Limited amplitude panel flutter with a temperature differential

Published:1994-04-18 Issue: Volume: Page:
ISSN:
Container-title:35th Structures, Structural Dynamics, and Materials Conference
language:
Short-container-title:

Author:

Hopkins Mark¹,Dowell Earl²

Affiliation:

1. USAF, Wright Lab., Wright-Patterson AFB, OH

2. Duke Univ., Durham, NC

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1994-1486

Reference9 articles.

1. Limit cycle oscillation of a fluttering cantilever plate

2. Bein, T., Friedmann, P., Zhong, X., and Nydick, I. "Hypersonic Flutter of a Curved Shallow Panel with AerodynamicHeating,"AIAA93-1318(34thSDM,omitted from proceedings).

3. Hopkins, M. A. "NonlinearEquations of Motion for aPanel SubjecttoExternalLoads,"WL-TM-93-308-FIBG, November 1993(AD# A273142).

4. Hopkins, M. A. "Responseof a CantileveredPlate in SupersonicFlow," WL-TM-94-XXX-FIBG,February 1994 (to be published).

5. Nonlinear oscillations of a fluttering plate.

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