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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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References | Additional Information

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

    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


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Article copyright: © Copyright 1968 American Mathematical Society