INTEGRATION OF PROPULSION SYSTEMS IN AIRFRAMES

Abstract

Contents: The influence of flight speed on the thrust calibration of a jet engine; Jet influence on V/STOL-aircraft in the transitional and high speed flight regime; Some studies into improvements in automatic throttle control; Engine airframe integration problems peculiar to aircraft configurations with nacelles mounted above the wing; Aircraft and propulsion operational considerations related to inlet design; A discussion of the use of thrust for control of VTOL aircraft; Reaction control system preliminary design considerations for a jet-lift research aircraft; Hot-gas ingestion and jet interference effects for jet V/STOL aircraft; Interaction between airframe- powerplant integration and hot gas ingestion for jet lift V/STOL transport aircraft.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1967
Accession Number
AD0672073

Entities

Organizations

  • AGARD

Tags

Communities of Interest

  • Air Platforms
  • Counter WMD
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Aircraft Equipment
  • Aircraft Industry
  • Aircrafts
  • Airframes
  • Boundary Layer
  • Center Of Gravity
  • Control Systems
  • Fluid Dynamics
  • Jet Aircraft
  • Jet Engines
  • Measurement
  • Pressure Distribution
  • Pressure Measurement
  • Research Aircraft
  • Short Takeoff Aircraft
  • Stabilization Systems

Fields of Study

  • Physics

Readers

  • Aerospace Engineering