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Flutter of an elastic plate under tension

Publication ,  Journal Article
Dowell, EH; Ventres, CS
Published in: AIAA J. (USA)
1977

A new interpretation of existing results is presented. Two-dimensional aerodynamic flow over a one-dimensional (infinitely wide) plate is considered. The effect is clarified of variations in plate bending stiffness on the flutter of a plate under a given tension, and vice versa. The conclusion is reached that for low-supersonic/transonic Mach numbers where flutter is most likely to occur, reducing bending stiffness reduces the dynamic pressure required for flutter

Duke Scholars

Published In

AIAA J. (USA)

Publication Date

1977

Volume

15

Issue

11

Start / End Page

1653 / 1655

Related Subject Headings

  • Aerospace & Aeronautics
  • 0913 Mechanical Engineering
  • 0905 Civil Engineering
  • 0901 Aerospace Engineering
 

Citation

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Dowell, E. H., & Ventres, C. S. (1977). Flutter of an elastic plate under tension. AIAA J. (USA), 15(11), 1653–1655.
Dowell, E. H., and C. S. Ventres. “Flutter of an elastic plate under tension.” AIAA J. (USA) 15, no. 11 (1977): 1653–55.
Dowell EH, Ventres CS. Flutter of an elastic plate under tension. AIAA J (USA). 1977;15(11):1653–5.
Dowell, E. H., and C. S. Ventres. “Flutter of an elastic plate under tension.” AIAA J. (USA), vol. 15, no. 11, 1977, pp. 1653–55.
Dowell EH, Ventres CS. Flutter of an elastic plate under tension. AIAA J (USA). 1977;15(11):1653–1655.

Published In

AIAA J. (USA)

Publication Date

1977

Volume

15

Issue

11

Start / End Page

1653 / 1655

Related Subject Headings

  • Aerospace & Aeronautics
  • 0913 Mechanical Engineering
  • 0905 Civil Engineering
  • 0901 Aerospace Engineering