The Linear Perturbation Theory of Axially Symmetric Compressible Flow with Application to the Effect of Compressibility on the Pressure Coefficient at the Surface of a Body of Revolution

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Document Details

Document Type
Technical Report
Publication Date
Jul 18, 1947
Accession Number
ADB804051

Entities

People

  • John G. Herriot

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamics
  • Aeronautics
  • Aircrafts
  • Coefficients
  • Compressible Flow
  • Compressive Properties
  • Fineness Ratio
  • Flow
  • Fluid Dynamics
  • Hydrodynamics
  • Incompressible Flow
  • Mach Number
  • Perturbation Theory
  • Perturbations
  • Slender Bodies
  • Stagnation Point
  • Three Dimensional