Tandem Helicopter Lateral Stability and Control

Abstract

The equations of motion, for lateral-directional dynamic stability and response of tandem helicopters in forward flight, are formulated. Theoretical expressions are developed for the various stability derivatives, and the results of preliminary calculations for an HUP type aircraft are discussed.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1956
Accession Number
AD0119202

Entities

People

  • Edward Seckel
  • Gerald Graziani

Organizations

  • Princeton University

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Engineering
  • Aeronautics
  • Aircrafts
  • Coefficients
  • Contracts
  • Control Sticks
  • Dynamic Response
  • Equations
  • Equations Of Motion
  • Government Procurement
  • Governments
  • Helicopters
  • Military Research
  • New York
  • Two Dimensional
  • United States
  • United States Government

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Control Systems Engineering.