HEAVY-LIFT TIP TURBOJET ROTOR SYSTEM. VOLUME 10. STABILITY AND CONTROL

Abstract

The report discusses the results of a stability and control analysis of a large crane-type helicopter powered by a tip-mounted turbojet system. Specification MIL-H-8501A was used as a guide for criteria. Specification criteria were met; however, for improvements in handling qualities, a stability augmentation system is recommended.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1965
Accession Number
AD0625822

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Space

DTIC Thesaurus Topics

  • Abstracts
  • Aircrafts
  • Airframes
  • Analog Computers
  • Angular Acceleration
  • Center Of Gravity
  • Classification
  • Engine Nacelles
  • Engineering
  • Engines
  • Equations Of Motion
  • Helicopters
  • Horizontal Stabilizers
  • Jet Aircraft
  • Sea Level
  • Specifications
  • Vehicles

Fields of Study

  • Physics

Readers

  • Aerospace Engineering