Transonic Fan/Compressor Rotor Design Study. Volume 1

Abstract

Volumes I through VI of 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 one 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. The report contains six volumes. Volume I contains primarily introduction and summary information plus details of a data match analysis of the base design. Volumes II through VI each contain design details for one of the series of five rotors.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1982
Accession Number
ADB069484

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
  • Computer Programs
  • Contracts
  • Engines
  • Geometry
  • Governments
  • Mach Number
  • Pressure Distribution
  • Static Pressure
  • Test And Evaluation
  • United States
  • Virtual Reality

Readers

  • Aerodynamics.
  • Business Analytics