Pulse Combustion Facility and Its Prliminary Application in Scramjet Research

Abstract

A new, more efficient and economical facility (which is capable of simulating flight Mach number less than 7) of pulse combustion and short duration (more than 30 ms) was conceived and built two years ago in CARDC, based on our original experience in short duration techniques for simulating exhaust plumes at high altitude. Preliminary experimental results from hundreds of tests of combustor and model engine with fuel of hydrogen and hydrocarbon demonstrate that this kind of facility is suitable for scramjet research.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 2002
Accession Number
ADA409258

Entities

People

  • Le Jialing
  • Liu Weixiong
  • Tan Yu
  • Wei He

Organizations

  • China Aerodynamics Research and Development Center

Tags

Communities of Interest

  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Autoignition
  • Chemical Reactions
  • Combustion
  • Combustors
  • Engines
  • Flow
  • Flow Rate
  • High Altitude
  • Ignition
  • Mass Flow
  • Pressure Measurement
  • Ramjet Engines
  • Shock Tunnels
  • Supersonic Combustion Ramjet Engines
  • Test Facilities
  • Two Dimensional
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Internal Combustion Engine (ICE) Technology.
  • Systems Analysis and Design