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Flutter of infinitely long plates and shells -- 2

Publication ,  Journal Article
Dowell, EH
Published in: AIAA Journal
1966

Aeroelastic stability of infinitely long, isotropic cylinder with outer surface exposed to inviscid flow is re-examined; cylinder behavior is described by shell equations of Goldenvieser, whereas aerodynamic forces are described by classical linearized potential theory; extensive numerical results for flutter velocity (and dynamic pressure) indicate effects of Mach number, thickness -- radius ratio, and density, or mass ratio; important consequence of present study is indication that aerodynamic loading on cylinder is of "slender body" type when axial wavelength is large compared to circumferential wavelength; it may be expected that similar result will hold for cylinders of finite length.

Duke Scholars

Published In

AIAA Journal

Publication Date

1966

Volume

4

Issue

9

Start / End Page

1510 / 1518

Related Subject Headings

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

Citation

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ICMJE
MLA
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Dowell, E. H. (1966). Flutter of infinitely long plates and shells -- 2. AIAA Journal, 4(9), 1510–1518.
Dowell, E. H. “Flutter of infinitely long plates and shells -- 2.” AIAA Journal 4, no. 9 (1966): 1510–18.
Dowell EH. Flutter of infinitely long plates and shells -- 2. AIAA Journal. 1966;4(9):1510–8.
Dowell, E. H. “Flutter of infinitely long plates and shells -- 2.” AIAA Journal, vol. 4, no. 9, 1966, pp. 1510–18.
Dowell EH. Flutter of infinitely long plates and shells -- 2. AIAA Journal. 1966;4(9):1510–1518.

Published In

AIAA Journal

Publication Date

1966

Volume

4

Issue

9

Start / End Page

1510 / 1518

Related Subject Headings

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