Aerodynamic boundary layer effects on flutter and damping of plates
Publication
, Journal Article
Dowell, EH
Published in: Journal of Aircraft
January 1, 1973
A previously developed shear flow model for describing the aerodynamic pressures on a moving flexible wall in a boundary layer type flow is utilized to perform stability (flutter) and response analyses for elastic plates. Results for flutter boundaries and damping in the subflutter range are presented and compared to available experimental data. Agreement between theory and experiment is generally good except for damping at low supersonic Mach numbers. © 1973, American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
Duke Scholars
Published In
Journal of Aircraft
DOI
ISSN
0021-8669
Publication Date
January 1, 1973
Volume
10
Issue
12
Start / End Page
734 / 738
Related Subject Headings
- Aerospace & Aeronautics
- 40 Engineering
- 09 Engineering
Citation
APA
Chicago
ICMJE
MLA
NLM
Dowell, E. H. (1973). Aerodynamic boundary layer effects on flutter and damping of plates. Journal of Aircraft, 10(12), 734–738. https://doi.org/10.2514/3.60298
Dowell, E. H. “Aerodynamic boundary layer effects on flutter and damping of plates.” Journal of Aircraft 10, no. 12 (January 1, 1973): 734–38. https://doi.org/10.2514/3.60298.
Dowell EH. Aerodynamic boundary layer effects on flutter and damping of plates. Journal of Aircraft. 1973 Jan 1;10(12):734–8.
Dowell, E. H. “Aerodynamic boundary layer effects on flutter and damping of plates.” Journal of Aircraft, vol. 10, no. 12, Jan. 1973, pp. 734–38. Scopus, doi:10.2514/3.60298.
Dowell EH. Aerodynamic boundary layer effects on flutter and damping of plates. Journal of Aircraft. 1973 Jan 1;10(12):734–738.
Published In
Journal of Aircraft
DOI
ISSN
0021-8669
Publication Date
January 1, 1973
Volume
10
Issue
12
Start / End Page
734 / 738
Related Subject Headings
- Aerospace & Aeronautics
- 40 Engineering
- 09 Engineering