A METHOD OF CALCULATING QUASI TWO-DIMENSIONAL FLOWS THROUGH CASCADES,

Abstract

Details are given of a procedure to compute the effect of varying axial velocity on the cascade performance of an axial flow compressor blade row. The relevant equations and the procedure of solution are given. Details are given of a computing program to carry out the calculations. The program is written in Fortran IV and is in three parts. Data cards giving details of the flow geometry have to be punched for the first part only. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1967
Accession Number
AD0656428

Entities

People

  • Ramani Mani

Organizations

  • California Institute of Technology

Tags

DTIC Thesaurus Topics

  • Axial Flow
  • Axial Flow Compressor Blades
  • Axial Flow Compressors
  • Compressor Blades
  • Compressors
  • Equations
  • Flow
  • Geometry
  • Mathematics
  • Two Dimensional
  • Two Dimensional Flow

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Computer Science/Computer Engineering/Data Science/Digital Signal Processing.
  • Fluid Dynamics.