Generalized aerodynamic forces on a flexible cylindrical shell undergoing transient motion
Author:
E. H. Dowell
Journal:
Quart. Appl. Math. 26 (1968), 343-353
DOI:
https://doi.org/10.1090/qam/99848
MathSciNet review:
QAM99848
Full-text PDF Free Access
References |
Additional Information
E. H. Dowell and S. E. Widnall, Generalized aerodynamic forces on an oscillating cylindrical shell, Quart. Appl. Math., 24, 1–17 (1966)
E. H. Dowell and S. E. Widnall, Generalized aerodynamic forces on an oscillating cylindrical shell: Subsonic and supersonic flow, AIAA Journal (4) 4 607–610 (April 1966)
S. E. Widnall and E. H. Dowell, Aerodynamic forces on an oscillating cylindrical duct with an internal flow, J. Sound Vib., (1) 6, 113–127 (1967)
D. G. Randall, Supersonic flow past quasi-cylindrical bodies of almost circular cross-section, ARC R. and M. No. 3067 (1958)
R. Stearman, Research on panel flutter of cylindrical shells, Midwest Research Institute, AFOSR Report 64–0074 (1964)
E. H. Dowell, Generalized aerodynamic forces on a flexible plate undergoing transient motion, Quart. Appl. Math.24, 331–338 (1967)
- Raymond L. Bisplinghoff and Holt Ashley, Principles of aeroelasticity, John Wiley and Sons, Inc., New York-London, 1962. MR 0151036
Bateman Manuscript Project, Tables of integral transforms, Vol. 1, McGraw-Hill, New York, 1954
E. H. Dowell and S. E. Widnall, Generalized aerodynamic forces on an oscillating cylindrical shell, Quart. Appl. Math., 24, 1–17 (1966)
E. H. Dowell and S. E. Widnall, Generalized aerodynamic forces on an oscillating cylindrical shell: Subsonic and supersonic flow, AIAA Journal (4) 4 607–610 (April 1966)
S. E. Widnall and E. H. Dowell, Aerodynamic forces on an oscillating cylindrical duct with an internal flow, J. Sound Vib., (1) 6, 113–127 (1967)
D. G. Randall, Supersonic flow past quasi-cylindrical bodies of almost circular cross-section, ARC R. and M. No. 3067 (1958)
R. Stearman, Research on panel flutter of cylindrical shells, Midwest Research Institute, AFOSR Report 64–0074 (1964)
E. H. Dowell, Generalized aerodynamic forces on a flexible plate undergoing transient motion, Quart. Appl. Math.24, 331–338 (1967)
R. L. Bisplinghoff and H. Ashley, Principles of aeroelasticity, John Wiley and Sons, New York, 1962
Bateman Manuscript Project, Tables of integral transforms, Vol. 1, McGraw-Hill, New York, 1954
Additional Information
Article copyright:
© Copyright 1968
American Mathematical Society