Investigation of Velocity Field Behind Low-Flying Wing with Fuselage,

Abstract

This article proposes a method for investigation of the velocity field behind a low-flying wing with fuselage. The value of the velocity field is necessary in calculating the aerodynamic characteristics of the tail assembly of aircraft which use the screen effect.

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Document Details

Document Type
Technical Report
Publication Date
May 11, 1977
Accession Number
ADA045073

Entities

People

  • L. G. Tsvetkov
  • M. K. Bochin

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Air Force
  • Aircrafts
  • All Wing Aircraft
  • Foreign Technology
  • Fuselages
  • Graphics
  • Stratified Fluids
  • Tail Assemblies
  • Translations

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Sensor Fusion and Tracking Systems.