Turbine Engine Variable Cycle Selection Program Summary.

Abstract

A systematic engine/airframe evaluation procedure was developed and used to assess interactions for fixed and variable geometry engine concepts in tactical aircraft. The evaluation procedure provides a rapid and inexpensive technique for evaluations of advanced engine concepts for extensive matrices of potential aircraft maneuverability and multi-mission requirements. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1977
Accession Number
ADA043408

Entities

People

  • F. C. Glaser
  • W. B. Weber

Organizations

  • McDonnell Aircraft Corporation

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air
  • Air Force
  • Aircraft Design
  • Aircrafts
  • Airframes
  • Combinatorial Analysis
  • Computer Programs
  • Fighter Aircraft
  • Geometry
  • Jet Aircraft
  • Jet Engines
  • Mach Number
  • Propulsion Systems
  • Turbine Components
  • Turbines
  • Turbofan Engines
  • Turbojet Engines

Readers

  • Aerospace Engineering
  • Systems Analysis and Design