Generalized aerodynamic forces on a flexible plate undergoing transient motion
Author:
Earl H. Dowell
Journal:
Quart. Appl. Math. 24 (1967), 331-338
DOI:
https://doi.org/10.1090/qam/99912
MathSciNet review:
QAM99912
Full-text PDF Free Access
Abstract |
References |
Additional Information
Abstract: The aerodynamic forces on a flexible plate embedded in a rigid half-space, undergoing arbitrary temporal and spatial motion are determined.
H. J. Cunningham, Flutter analysis of flat rectangular panels based on three-dimensional supersonic potential flow, AIAA Journal (8) 1, 1795–1801 (August 1963)
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, Q. 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)
R. L. Bisplinghoff, H. Ashley and R. L. Halfman, Aeroelasticity, Addison-Wesley, Cambridge, Mass., 1955
H. J. Cunningham, Flutter analysis of flat rectangular panels based on three-dimensional supersonic potential flow, AIAA Journal (8) 1, 1795–1801 (August 1963)
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, Q. 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)
R. L. Bisplinghoff, H. Ashley and R. L. Halfman, Aeroelasticity, Addison-Wesley, Cambridge, Mass., 1955
Additional Information
Article copyright:
© Copyright 1967
American Mathematical Society
