Engine-Airframe Integration for Rotorcraft.

Abstract

These lectures address numerous engine airframe integration aspects relating to rotor wing aircraft. Various areas of engine airframe integration, including the impact of advanced engine design variables to specific propulsion subsystems, i.e. engine air inlets, are discussed. Other propulsion system integration aspects such as engine/rotor/drive system torsional stability and transient response are also addressed.

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1986
Accession Number
ADA171297

Entities

Organizations

  • AGARD

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Human Systems
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircraft Equipment
  • Aircraft Industry
  • Aircrafts
  • Airframes
  • Fixed Wing Aircraft
  • Fluid Dynamics
  • Heat Transfer
  • Material Degradation Processes
  • Materials Science
  • Materials Testing
  • Mechanics
  • Rotary Wing Aircraft
  • Test And Evaluation
  • Test Methods
  • Transport Aircraft
  • Two Dimensional
  • Warning Systems

Fields of Study

  • Physics

Readers

  • Academic Conference Management
  • Aerospace Engineering