Aircraft Engines (Selected Articles)

Abstract

;Contents: The effect of the form of an active gas jet on the characteristics of a gas ejector with short mixing chamber; Calculation of the maximum degree of compression of an ejector; The rational method of selecting parameters and calculating single-stage gas turbines; A generalization of the results of measurements of the fineness of fuel atomization of mechanical and air-mechanical injectors of the pressure-jet type; Calculation of temperature field in a cooled turbine blade with longitudinal cooling channels; Turbulence in the zone of interplay of jetstreams with the flow.

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Document Details

Document Type
Technical Report
Publication Date
May 07, 1971
Accession Number
AD0727175

Entities

People

  • A. V. Sharapov
  • I. I. Kalmykov
  • I. N. Dyatlov
  • V. A. Strunkin
  • Yu. A. Bordovitsyn

Organizations

  • Air Force Systems Command

Tags

Communities of Interest

  • Energy and Power Technologies
  • Sensors

DTIC Thesaurus Topics

  • Accuracy
  • Air Flow
  • Air Force
  • Combustion
  • Combustion Products
  • Exhaust Gases
  • Gas Flow
  • Gas Turbines
  • Geometric Forms
  • Heat Transfer
  • Heat Transmission
  • Measurement
  • Turbine Blades
  • Turbines
  • Turbojet Engines
  • Turboprop Engines
  • Turbulent Mixing

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Internal Combustion Engine (ICE) Technology.