WIND TUNNEL TEST OF 1/7 SCALE MODEL OV-1

Abstract

Wind tunnel tests were conducted on a 1/7 scale model of the OV-1 airplane to determine the power-off drag, lift, and pitching moment coefficients of the model and its various components. Significant drag differences were measured between production canopy and nacelle configurations and streamlined fuselage and nacelle configurations, but are not considered applicable. No other significant drag differences were measured.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1965
Accession Number
AD0630924

Entities

People

  • Fred W. Shepheard

Organizations

  • Grumman

Tags

Communities of Interest

  • Air Platforms
  • Biomedical
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Airplanes
  • Army Aviation
  • Contracts
  • Engineering
  • Government Procurement
  • Military Research
  • Naval Air Stations
  • New York
  • Production
  • Scale Models
  • Systems Engineering
  • Test And Evaluation
  • United States
  • Wind Tunnel Models
  • Wind Tunnel Tests
  • Wind Tunnels

Fields of Study

  • Agricultural and Food sciences
  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Solar Physics