Model of Aircraft for Testing in a Wind Tunnel,

Abstract

This invention is the model of an aircraft for testing in wind tunnel. Its housing contains drain channels which are withdrawn into the inner cavity of the model's body, which is connected by a pipe with a source of liquid and source of compressed air. (Russian translations)

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Document Details

Document Type
Technical Report
Publication Date
Dec 30, 1986
Accession Number
ADA176095

Entities

People

  • L. V. Novikov
  • N. F. Sterlikov

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air
  • Aircrafts
  • Compressed Air
  • Conductive Liquids
  • Electrodes
  • Foreign Technology
  • Inventions
  • Law
  • Liquids
  • Materials
  • Pressure Distribution
  • Schematic Diagrams
  • Translations
  • Wind Tunnels

Readers

  • Aerodynamics/Aeronautics.
  • Combustion and Flow Dynamics.
  • Hydraulic Engineering.