Experimental Investigation of Supersonic Combustion of Liquid Hydrocarbon Fuel Using Barbotage in the Aeroramp Configuration at M=2.5

Abstract

This report results from a contract tasking TsAGl as follows: The contractor will investigate combustion of kerosene using barbotage by hydrogen and air in the aeroramp configuration at M=2.5 as described in his proposal dated 1 Jun 98.

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Document Details

Document Type
Technical Report
Publication Date
Aug 10, 1999
Accession Number
ADA368781

Entities

People

  • Vladimir Sabelnikov

Tags

Communities of Interest

  • Air Platforms
  • Materials and Manufacturing Processes
  • Sensors

DTIC Thesaurus Topics

  • Air Force
  • Combustion
  • Combustion Products
  • Combustors
  • Contracts
  • Heat Flux
  • Hydrocarbon Fuels
  • Hydrocarbons
  • Payload
  • Pressure Distribution
  • Pressure Measurement
  • Scientific Research
  • Static Pressure
  • Supersonic Combustion
  • Supersonic Flow
  • Test Facilities
  • Three Dimensional

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Internal Combustion Engine (ICE) Technology.
  • Technical Research and Report Writing.

Technology Areas

  • Hypersonics