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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

Weak Solution Jump Condition Transonic Flow Wall Boundary Condition Outer Solution 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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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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