HEAVY-LIFT TIP TURBOJET ROTOR SYSTEM. VOLUME 9. PERFORMANCE ANALYSIS

Abstract

The report presents a performance and characteristics summary of the Model 1108 tip turbojet-powered heavylift helicopter. The configuration was selected from a parametric analysis (USAAVLABS Technical Report 64-68B). Standard performance methods are used, modified where necessary by factors peculiar to tip turbojet propulsion.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1965
Accession Number
AD0625821

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Abstracts
  • Aerodynamic Characteristics
  • Aircrafts
  • Blade Tips
  • Engines
  • Equations
  • Flight Speeds
  • Fuel Systems
  • Ground Effect
  • Helicopters
  • Jet Aircraft
  • Mach Number
  • Parametric Analysis
  • Sea Level
  • Security
  • Standards
  • Turbojet Engines

Fields of Study

  • Physics

Readers

  • Aerospace Engineering