EXPERIMENTAL AND DESIGN STUDIES FOR TURBO-RAMJET COMBINATION ENGINE. VOLUME 3 - DATA

Abstract

The data necessary for the calculations relating to the performance characteristics of the turbofan-ramjet combination engine are presented. The geometric and thermodynamic characteristics of the SNECMA TF 106 turbofan are brought together. The numerical values of the various parameters, coefficients and functions defining the efficiencies of the different parts of the engine, as well as the geometrical characteristics peculiar to the combination engine are given.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1966
Accession Number
AD0486377

Entities

People

  • A. Gozlan
  • M. Ravel
  • P. Chaulin

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Flow
  • Air Force
  • Air Force Facilities
  • Annular Flow
  • Calorific Value
  • Chambers
  • Combustion
  • Combustion Chambers
  • Engines
  • Flame Holders
  • Flight
  • Flow
  • Mach Number
  • Ramjet Engines
  • Static Pressure
  • Turbines
  • Turbofan Engines

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Combustion and Flow Dynamics.
  • Electromagnetic Wave Scattering and Antenna Radiation Engineering