Internal Aerodynamics Manual. Appendix

Abstract

The report is organized into six sections and consists of tabulations that will facilitate theoretical thermodynamic calculations. These sections of the Appendix are: basic thermodynamic relationships, normal shock wave parameters, two-dimensional shock wave parameters, three-dimensional shock wave analysis,corrected weight flow parameters, and parameters for thrust calculation.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1970
Accession Number
AD0723841

Tags

Communities of Interest

  • Sensors

DTIC Thesaurus Topics

  • Aircrafts
  • Boundary Layer
  • Computational Fluid Dynamics
  • Control Systems
  • Differential Equations
  • Equations
  • Flow Fields
  • Geometry
  • Insensitive Explosives
  • Plastic Explosives
  • Pressure Distribution
  • Propulsion Systems
  • Skin Friction
  • Static Pressure
  • Three Dimensional
  • Turbojet Engines
  • Two Dimensional

Readers

  • Aerospace Engineering
  • Business Analytics
  • Combustion Dynamics and Shock Wave Physics.