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
APA
Chicago
ICMJE
MLA
NLM
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