Quarterly of Applied Mathematics

Quarterly of Applied Mathematics

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

   
 
 

 

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
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  • [1] E. H. Dowell and S. E. Widnall, Generalized aerodynamic forces on an oscillating cylindrical shell, Quart. Appl. Math., 24, 1-17 (1966)
  • [2] 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)
  • [3] 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)
  • [4] D. G. Randall, Supersonic flow past quasi-cylindrical bodies of almost circular cross-section, ARC R. and M. No. 3067 (1958)
  • [5] R. Stearman, Research on panel flutter of cylindrical shells, Midwest Research Institute, AFOSR Report 64-0074 (1964)
  • [6] E. H. Dowell, Generalized aerodynamic forces on a flexible plate undergoing transient motion, Quart. Appl. Math.24, 331-338 (1967)
  • [7] Raymond L. Bisplinghoff and Holt Ashley, Principles of aeroelasticity, John Wiley and Sons, Inc., New York-London, 1962. MR 0151036
  • [8] Bateman Manuscript Project, Tables of integral transforms, Vol. 1, McGraw-Hill, New York, 1954


Additional Information

DOI: https://doi.org/10.1090/qam/99848
Article copyright: © Copyright 1968 American Mathematical Society

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