Flow Problems in Turbomachines.

Abstract

A brief discussion is given of the work done on the three problems studied during the period covered by this report. The problems considered are: (1) transonic flow through heavily loaded cascades, (2) transonic flow through a three-dimensional compressor rotor, and (3) supersonic flow with a turbulent boundary layer at a ramp. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Apr 15, 1983
Accession Number
ADA128675

Entities

People

  • Arthur F. Messiter
  • Thomas C. Adamson Jr.

Organizations

  • University of Michigan

Tags

Communities of Interest

  • Air Platforms
  • Space

DTIC Thesaurus Topics

  • Boundary Layer
  • Channel Flow
  • Coordinate Systems
  • Engineering
  • Equations
  • Flow Fields
  • Inviscid Flow
  • Leading Edges
  • Mach Number
  • Mechanical Engineering
  • Mechanics
  • Military Research
  • Pressure Distribution
  • Pressure Measurement
  • Shear Stresses
  • Three Dimensional
  • Turbulent Boundary Layer

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Fluid Mechanics and Fluid Dynamics.
  • Technical Research and Report Writing.

Technology Areas

  • Hypersonics