Transonic Fan/Compressor Rotor Design Study. Volume 6

Abstract

This report describes the aerodynamic design of a series of five transonic rotors all parametrically related to a baseline design documented in Technical Report AFAPL-TR-79-2078. Each of the five designs deviate from the base line, in so far as practical, by a variation of parameter only. The parametric variations are specified at the rotor tip. The original hub characteristics were preserved to the maximum extent practical. The varied parameter was adjusted along the span.

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1982
Accession Number
ADB069628

Entities

People

  • D. E. Parker
  • M. R. Simonson

Organizations

  • General Electric

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Air Force
  • Air Force Facilities
  • Aircraft Engines
  • Base Lines
  • Commerce
  • Compressor Rotors
  • Governments
  • Leading Edges
  • Mach Number
  • Plastic Explosives
  • Pressure Distribution
  • Static Pressure
  • Test And Evaluation
  • Two Dimensional
  • United States Government
  • Virtual Reality

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Computer Science.