HEAVY-LIFT TIP TURBOJET ROTOR SYSTEM. VOLUME 1

Abstract

The study of a tip-turbojet-powered rotor system for a heavy-lift helicopter, which is presented in thirteen volumes, is summarized. Included under this general subject are studies on parametric design, performance, structures and dynamics, wind tunnel, preliminary design, weight and balance, stability, and power plant.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1965
Accession Number
AD0625818

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircraft Equipment
  • Aircrafts
  • Airframes
  • Auxiliary Power Units
  • Boundary Layer
  • Dynamic Loads
  • Engines
  • Fuel Systems
  • Generators
  • Geometry
  • Helicopters
  • Jet Aircraft
  • Materials
  • Resonant Frequency
  • Turbines
  • Turbojet Engines
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Business Analytics