Gas-Dynamic Verification Calculation of Axial-Flow Multistage Compressors on EDC,

Abstract

An algorithm for testing the gas dynamic design of axial-flow compressors, particularly in the final adjustment phase, is proposed. Particularly well suited for calculating the parameters of blade rings, the procedure is suitable for use in the design phase if data on the loss coefficients in empirical formulas have been established. (Author)

Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1972
Accession Number
AD0753519

Entities

People

  • A. P. Tunakov
  • S. G. Ibragimov

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Algorithms
  • Axial Flow
  • Axial Flow Compressors
  • Coefficients
  • Compressors
  • Flow
  • Pneumatic Equipment
  • Rotary Compressors
  • Verification

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Approximation Theory.