Computer Program for Relaxation Solutions of the Nonlinear Small-Disturbance Equations for Transonic Flow in an Axial Compressor Blade Row.

Abstract

This report contains a description of a computer program for calculating the three-dimensional transonic flow through a compressor blade row, in the nonlinear small-disturbance approximation, and for subsonic values of the inlet relative Mach number at the blade tip. The problem formulation is reviewed briefly; following this, a description of the program is given together with a listing and sample case. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1978
Accession Number
ADA053744

Entities

People

  • William J. Rae

Organizations

  • Calspan

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Force
  • Blade Tips
  • Boundaries
  • Compressor Blades
  • Compressors
  • Computer Programs
  • Computers
  • Flow
  • Geometry
  • Intervals
  • Leading Edges
  • Mach Number
  • Plastic Explosives
  • Shock
  • Three Dimensional
  • Transonic Flow
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Business Analytics
  • Finite Element Method (FEM) for solving Partial Differential Equations (PDEs)