Quarterly of Applied Mathematics

Quarterly of Applied Mathematics

Online ISSN 1552-4485; Print ISSN 0033-569X

   
 
 

 

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
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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.


References [Enhancements On Off] (What's this?)

  • [1] H. J. Cunningham, Flutter analysis of flat rectangular panels based on three-dimensional supersonic potential flow, AIAA Journal (8) 1, 1795-1801 (August 1963)
  • [2] Bateman Manuscript Project, Tables of integral transforms, Vol. 1, McGraw-Hill, New York, 1954
  • [3] E. H. Dowell and S. E. Widnall, Generalized aerodynamic forces on an oscillating cylindrical shell, Q. Appl. Math. 24, 1-17 (1966)
  • [4] 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)
  • [5] R. L. Bisplinghoff, H. Ashley and R. L. Halfman, Aeroelasticity, Addison-Wesley, Cambridge, Mass., 1955


Additional Information

DOI: https://doi.org/10.1090/qam/99912
Article copyright: © Copyright 1967 American Mathematical Society

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