Fan-in-Fuselage Advanced Antitorque System

Abstract

The information contained in this report is a result of study, analysis and design conducted to determine the performance of a helicopter with a fan-in-fuselage antitorque and yaw control system, as compared with the performance of the same basic helicopter with a tail rotor.

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1974
Accession Number
ADA005049

Entities

People

  • Carroll R. Akeley
  • George W. Carson

Organizations

  • Kaman Corporation

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Ground and Sea Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Aircrafts
  • Airfoils
  • Airframes
  • Contracts
  • Control Systems
  • Engineers
  • Exhaust Gases
  • Flow Rate
  • Fuselages
  • Helicopters
  • Internal Pressure
  • Rotary Wing Aircraft
  • Shrouded Propellers
  • Standards
  • Three Dimensional
  • Vulnerability

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Control Systems Engineering.
  • Geodesy