Generalized aerodynamic forces on oscillating cylindrical shell -- Subsonic and supersonic flow

Journal Article (Academic Article)

Mathematical and numerical solution is presented for problem of determining aerodynamic forces on harmonically oscillating, cylindrical shell within framework of classical, linearized, potential flow theory; subsonic speeds are emphasized; method of solution is outlined, and numerical results are presented; comparisons of results are made with those of (generalized) "slender body" theory to indicate where this simpler theory may be used with confidence. (See also Quarterly of Applied Mathematics v 24 n 1 Apr 1966 p 1-17)

Duke Authors

Cited Authors

  • Dowell, EH; Widnall, SE

Published Date

  • 1966

Published In

  • AIAA Journal

Volume / Issue

  • 4 / 4

Start / End Page

  • 607 - 610