An Introduction to Dynamic Derivatives (3) Methods of Oscillating Models in Pitch and Yaw in a 530 by 810 Millimetre Transonic Wind Tunnel.

Abstract

Mechanisms are considered which allow models to be oscillated in pitch and yaw during wind tunnel tests to measure dynamic derivatives. Types of pivots, motion producing linkages and connecting linkages are described as applicable in a 530 by 810 millimeter Transonic Tunnel. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1979
Accession Number
ADA089377

Entities

People

  • G. F. Forsyth

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Sensors
  • Space

DTIC Thesaurus Topics

  • Accuracy
  • Aeronautics
  • Aircrafts
  • Bearings
  • Boundary Layer
  • Fluid Dynamics
  • Fluid Mechanics
  • Measurement
  • Resonant Frequency
  • Skull
  • Strain Gages
  • Test Facilities
  • Transonic Wind Tunnels
  • Two Dimensional
  • Wind Tunnel Models
  • Wind Tunnel Tests
  • Wind Tunnels

Readers

  • Aerodynamics/Aeronautics.
  • Radar Systems Engineering.
  • Theoretical Analysis.