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Low temperature nonequilibrium plasma production for ignition and combustion control in hypersonic flow

  • Moscow Institute of Physics and Technology

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

Novel experimental scheme for investigation of threshold shift at high temperatures under the action of high-voltage nanosecond discharge has been developed. Experimental technique to control electrical parameters in nanosecond time scale and ignition processes in microsecond time scale was proposed. The ignition threshold shifts for different mixtures, gas pressures and temperatures were obtained experimentally. Ignition delay dependence upon temperature, high voltage amplitude and energy release into the discharge was determined for H2-air and CH4-air mixtures diluted with argon.

Original languageEnglish
Title of host publication38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
ISBN (Print)9781624101151
DOIs
Publication statusPublished - 1 Jan 2002
Externally publishedYes
Event38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2002 - Indianapolis, IN, United States
Duration: 7 Jul 200210 Jul 2002

Publication series

Name38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Conference

Conference38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2002
Country/TerritoryUnited States
CityIndianapolis, IN
Period7/07/0210/07/02

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