EXPERIMENTAL AND DESIGN STUDIES FOR TURBO-RAMJET COMBINATION ENGINE. VOLUME 1 - SPECIFICATIONS AND PERFORMANCE

Abstract

Contents: GENERAL DESCRIPTION; DEFINITION OF THE X 81 COMBINED ENGINE; PERFORMANCE CHARACTERISTICS--Sea level static; flight air mass flow; flight without afterburning; flight with afterburning; Influence of the air inlet total pressure recovery; Influence of the nozzle thrust coefficient; Influence of air bleed; OVERALL DIMENSIONS - WEIGHT; INSTALLATION - HANDLING; AND COMBUSTION TESTS.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1966
Accession Number
AD0486375

Entities

People

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

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Afterburning
  • Air Flow
  • Air Force
  • Altitude
  • Combustion
  • Combustion Chambers
  • Engines
  • Flow
  • Gas Turbines
  • Generators
  • Ignition Lag
  • Mach Number
  • Ramjet Engines
  • Sea Level
  • Specifications
  • Turbines
  • Turbofan Engines

Readers

  • Aerospace Test and Evaluation
  • Combustion and Flow Dynamics.