An Introduction to Dynamic Derivatives (2) The Equations of Motion for Wind Tunnel Pitch-Yaw Oscillation Rigs.

Abstract

The equations of motion are developed for a simplified free flight pitch-yaw system and for spring-mounted and rigidly-driven wind tunnel systems. For the spring-mounted system both initial displacement and forced-oscillation conditions are examined. A simplified cable towed system is also derived. A bibliography is included. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1978
Accession Number
ADA071643

Entities

People

  • G. F. Forsyth

Tags

Communities of Interest

  • Air Platforms
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aeronautics
  • Aircraft Industry
  • Aircrafts
  • Atmospheric Motion
  • Birds
  • Equations
  • Equations Of Motion
  • Flight
  • Fluid Dynamics
  • Free Flight
  • Measurement
  • Mechanical Engineering
  • Mechanics
  • Military Aircraft
  • Test Facilities
  • United States
  • Wind Tunnels

Readers

  • Aerodynamics/Aeronautics.
  • Control Systems Engineering.
  • Electrical Engineering