WIND TUNNEL TEST STUDY

Abstract

The test results are discussed in the following order: (a) Devices to reduce the nose up pitching moment in forward flight. (b) Determination of trim points, and stability and control work. (c) Miscellaneous tests.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1958
Accession Number
AD0658996

Entities

Organizations

  • Stellantis North America (formerly Chrysler)

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Coefficients
  • Dynamic Pressure
  • Engineering
  • Flight
  • Flow
  • Flow Visualization
  • Fuselages
  • Ground Effect
  • Hovering
  • Models
  • National Security
  • Photographs
  • Propeller Blades
  • Propellers
  • Test Vehicles
  • Wind Tunnel Tests
  • Wind Tunnels

Readers

  • Aerodynamics/Aeronautics.
  • Technical Research and Report Writing.