HIGH SPEED AERODYNAMICS AND JET PROPULSIONS. VOLUME 10. AERODYNAMICS OF TURBINES COMPRESSORS

Abstract

Contents: Theory Of Two-Dimensional Flow Through Cascades--General treatment of incompressible inviscid two-dimensional cascade flow, and Methods of treating compressibility, high solidity, and viscous effects in two- dimensional cascades; Three-Dimensional Flow In A TurboMachines--Experimental techniques, Flow in cascades, The axial compressor stage, and The supersonic compressor; Early work on supersonic compressors, and Aerodynamic properties of supersonic compressors; Aerodynamic Design Of Axial Flow Turbines--Fundamental principles, Experimental data on performance, Three-dimensonal effects, and Turbine design; The Radial Turbine--Ideal flow through a radial turbine, and Real flow through a radial turbine; The Centrifugal Compressor--Blading interaction effects in turbines.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1964
Accession Number
AD0452271

Entities

People

  • W. R. Hawthorne

Organizations

  • Princeton University

Tags

Communities of Interest

  • Air Platforms
  • Ground and Sea Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Computational Fluid Dynamics
  • Flow Visualization
  • Fluid Dynamics
  • Fluid Flow
  • Gas Turbines
  • Heat Transfer
  • Hydrodynamics
  • Measurement
  • Mechanical Properties
  • Mechanics
  • Pressure Measurement
  • Rotor Blades (Turbomachinery)
  • Standing Waves
  • Telemetry Equipment
  • Test And Evaluation
  • Turbine Components

Fields of Study

  • Physics

Readers

  • Aerodynamics.

Technology Areas

  • Hypersonics