High Bypass Turbofan Component Development. Phase II. Detailed Design.

Abstract

A detailed aerodynamic, aeromechanical and mechanical design of the high bypass turbofan fan stage selected during Phase I of this program was satisfactorily completed. This fan design is the result of aero and aeromechanical iterations and trade-offs which achieved the objectives of meeting aerodynamic performance as well as the life and mechanical considerations of MIL-E-5007D. The resulting fan design compares very closely to the fan originally proposed. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1979
Accession Number
ADA082753

Entities

People

  • D. Weldon
  • H. Mauch
  • T. Oldakowski

Organizations

  • General Electric

Tags

DTIC Thesaurus Topics

  • Air Force
  • Aircraft Engines
  • Aircrafts
  • Aspect Ratio
  • Bird Strikes
  • Contracts
  • Fabrication
  • Fan Blades
  • Flow Fields
  • Foreign Object Damage
  • Frequency
  • Geometry
  • Guide Vanes
  • High Bypass Turbofans
  • Leading Edges
  • Test Facilities
  • Turbofan Engines

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Systems Analysis and Design