Calculation of the Aerodynamic Characteristics of a Twisted Jet

Abstract

The work presents the results of the experimental and calculation study of a twisted jet flowing from an axial-flow swirl vane of the blade type and from an axial-tangential blade and helical swirl vanes. It presents the basic structural parameters of the studied swirl vanes and the value of twist parameters.

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Document Details

Document Type
Technical Report
Publication Date
Jun 17, 1974
Accession Number
AD0781657

Entities

People

  • R. B. Akhmedov
  • T. E. Balagula

Tags

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Agreements
  • Air Flow
  • Air Force
  • Air Force Facilities
  • Axial Flow
  • Boundaries
  • Conductivity
  • Diameters
  • Dynamic Pressure
  • Equations
  • Experimental Data
  • Flow
  • Flow Fields
  • Foreign Technology
  • Static Pressure
  • Thermal Conductivity

Fields of Study

  • Physics

Readers

  • Aerodynamics.