Perturbation of Transonic Flow with Shocks

  • Mohamed Hafez

Abstract

Perturbation analysis is used to study transonic flows including nonlinear inviscid compressibility effects as in transonic small-disturbance theory, as well as perturbations of boundary conditions and flow parameters (e.g. Mach number M , angle of attack α, thickness ratio τ, wing aspect ratio AR, sweep angle Λ, reduced frequency ω, tunnel height H, etc.).

Keywords

Vortex Porosity Compressibility Line Source 

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Copyright information

© Springer Science+Business Media New York 1982

Authors and Affiliations

  • Mohamed Hafez
    • 1
  1. 1.NASA-Langley Research CenterThe George Washington UniversityHamptonUSA

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