WIND TUNNEL TEST STUDY

Abstract

The report includes information pertaining to the construction and testing of the CARV (Chrysler Aerial Research Vehicle). This wind tunnel test model was constructed and tested. The first part of the test program covered the following investigations: (a) Vane effectiveness in hovering. (b) Forward flight conditions for tandem configuration. (c) Forward flight conditions for abreast configuration. (d) Finding a method to reduce the positive pitching moment.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1958
Accession Number
AD0658995

Entities

Organizations

  • Stellantis North America (formerly Chrysler)

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Accuracy
  • Aeronautical Engineering
  • Distribution Curves
  • Dynamic Pressure
  • Engineering
  • Engineers
  • Measurement
  • Pressure Distribution
  • Pressure Measurement
  • Propellers
  • Sea Level
  • Standards
  • Test Vehicles
  • Tubes
  • Wind Tunnel Tests
  • Wind Tunnels
  • Wind Velocity

Readers

  • Aerodynamics/Aeronautics.
  • Systems Analysis and Design