AIR LOADS AND PRESSURE DISTRIBUTION ON A PARABOLIC ANTENNA MODEL

Abstract

A series of tests on a parabolic scanner model was conducted for the M.I.T. Lincoln Laboratory at the Wright Brothers Wind Tunnel at M.I.T. during the periods October 13, 1961, to January 2, 1962, and May 25 to June 1, 1962. The wind tunnel is a low subsonic velocity test facility with an elliptic test section measring 7 1/2 x 10 feet. The purpose of the experimental investigation was to determine the airloads - pitching, rolling and yawing moments, lift, drag, and sideforce - on a parabolic reflector with a simulated screen and a solid surface and to determine the pressure distribution on the solid surface reflector.

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Document Details

Document Type
Technical Report
Publication Date
Oct 30, 1962
Accession Number
AD0290512

Entities

People

  • Joseph Bicknell
  • Raffi Yeghiayan

Organizations

  • Massachusetts Institute of Technology

Tags

DTIC Thesaurus Topics

  • Aerodynamic Loading
  • Antennas
  • Coefficients
  • Diameters
  • Dynamic Pressure
  • Elevation
  • Ground Effect
  • Models
  • Pressure Distribution
  • Reflectors
  • Static Pressure
  • Symmetry
  • Tank Guns
  • Test Facilities
  • Wind
  • Wind Direction
  • Wind Tunnels

Readers

  • Aerodynamics/Aeronautics.
  • Phased Array Antenna Design.
  • Technical Research and Report Writing.