Flutter of infinitely long plates and shells -- 1
Publication
, Journal Article
Dowell, EH
Published in: AIAA Journal
1966
Aeroelastic stability of infinitely long panel of finite width with upper surface exposed to inviscid flow is examined; panel behavior is accounted for by small deflection plate theory, whereas aerodynamic forces acting on panel are described by classical linearized, potential theory; extensive numerical results have been obtained for flutter velocity (and dynamic pressure) indicating effects of Mach number, air/panel mass ratio, and viscous structural damping; comparison of results with those obtained by previous investigators for long, narrow panel (using more elaborate method that accounts for finite length) shows some discrepancy between two results.
Duke Scholars
Published In
AIAA Journal
Publication Date
1966
Volume
4
Issue
8
Start / End Page
1370 / 1377
Related Subject Headings
- Aerospace & Aeronautics
- 4012 Fluid mechanics and thermal engineering
- 4001 Aerospace engineering
- 0913 Mechanical Engineering
- 0905 Civil Engineering
- 0901 Aerospace Engineering
Citation
APA
Chicago
ICMJE
MLA
NLM
Dowell, E. H. (1966). Flutter of infinitely long plates and shells -- 1. AIAA Journal, 4(8), 1370–1377.
Dowell, E. H. “Flutter of infinitely long plates and shells -- 1.” AIAA Journal 4, no. 8 (1966): 1370–77.
Dowell EH. Flutter of infinitely long plates and shells -- 1. AIAA Journal. 1966;4(8):1370–7.
Dowell, E. H. “Flutter of infinitely long plates and shells -- 1.” AIAA Journal, vol. 4, no. 8, 1966, pp. 1370–77.
Dowell EH. Flutter of infinitely long plates and shells -- 1. AIAA Journal. 1966;4(8):1370–1377.
Published In
AIAA Journal
Publication Date
1966
Volume
4
Issue
8
Start / End Page
1370 / 1377
Related Subject Headings
- Aerospace & Aeronautics
- 4012 Fluid mechanics and thermal engineering
- 4001 Aerospace engineering
- 0913 Mechanical Engineering
- 0905 Civil Engineering
- 0901 Aerospace Engineering