Throttle Dependent Forces - A Primer

Abstract

This report is intended to provide an introduction to the broad area of throttle dependent forces for airbreathing aircraft, primarily subsonic to supersonic capable. Basic concepts and examples are presented for subsonic, supersonic and transonic inlet and nozzle applications. Experimental and analytical determination of throttle-dependent forces is discussed, including approaches and potential problems. A final reference section of basic definitions is included for completeness. key words: Aircraft, Exhaust nozzles, Inlets, Airbreathing propulsion, Subsonic, Transonic, Supersonic.

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1985
Accession Number
ADA162939

Entities

People

  • Douglas L. Bowers

Organizations

  • Wright Laboratory

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircraft Equipment
  • Aircraft Industry
  • Aircrafts
  • Airframes
  • Boundary Layer
  • Computational Fluid Dynamics
  • Computational Science
  • Jet Transport Aircraft
  • Pressure Distribution
  • Pressure Measurement
  • Propulsion Systems
  • Short Takeoff Aircraft
  • Simulators
  • Tactical Aircraft
  • Transonic Aircraft
  • Transport Aircraft
  • Turbines

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Aerospace Engineering
  • Library and Information Science

Technology Areas

  • Hypersonics