Supersonic Cascade Studies. Part 1. Passage Studies

Abstract

An experimental study was made of supersonic flow through various convergent and convergent-divergant passage configurations. The details of the flows were examined by means of total and static pressure surveys and Schlieren photographs and the effects of some changes in passage geometry on the characteristics of the passages were observed. Based on the tests, some design criteria were determined for supersonic passages capable of operating at high static pressure ratios. It was concluded that long and narrow convergent- divergent passages are capable of producing a significant pressure rise without extensive separation in the divergent region. However, the values of obtainable pressure rise appears to be substantially lower than anticipated by early designers of supersonic compressor cascades.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1961
Accession Number
ADA280286

Entities

People

  • Andrew A. Fejer
  • George L. Heath

Organizations

  • University of Toledo

Tags

Communities of Interest

  • Air Platforms
  • Space

DTIC Thesaurus Topics

  • Air Force
  • Boundary Layer
  • Boundary Layer Flow
  • Boundary Layer Transition
  • Boundary Layer Trips
  • Compressors
  • Computational Fluid Dynamics
  • Fluid Dynamics
  • Heat Transfer
  • Laminar Boundary Layer
  • Pressure Distribution
  • Reynolds Number
  • Stagnation Pressure
  • Surface Temperature
  • Turbulent Flow
  • Turbulent Mixing
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Combustion Dynamics and Shock Wave Physics.
  • Computational Fluid Dynamics (CFD)

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow