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Deflagration-to-detonation control by non-equilibrium gas discharges and its applications for pulsed detonation engine

  • Moscow Institute of Physics and Technology

Research output: Contribution to conferencePaperpeer-review

Abstract

In the present work we propose to use the non-equilibrium gas discharge plasma for preliminary gas excitation and reduction of the chemical induction time in the mixture. Synchronization of the ignition of different parts of the gas using gas discharge excitation may lead to sufficient reduction of the DDT length and improvement the efficiency of the detonation engines. The ignition dynamics under the action of nanosecond discharge (up to 100 kV voltage, up to 10 atm initial gas pressure, 300-2000 K temperature range) is discussed both for thermally equilibrium and nonequilibrium plasma. The main processes responsible for the ignition initiation and control are determined for different regimes. Measurements of ignition delay time in lean methane-air, propane-air, hexane-air and decane-air mixtures were performed in the wide pressure range from 3 to 500 atmospheres and temperatures from 750 to 1800 K using reflected shock wave technique. Ignition delay times were determined using emission at 306 nm OH(X2II ← A2Σ+) and absorption diagnostics at 3.3922 μm (component F1(2) (n 3 = 1) ← F2(2)(n3 = 0) of P(7) line of n3 mode of CH4 molecule). The experimental data obtained were compared with the calculated by different kinetics mechanisms.

Original languageEnglish
Pages11168-11179
Number of pages12
DOIs
Publication statusPublished - 1 Jan 2004
Externally publishedYes
Event42nd AIAA Aerospace Sciences Meeting and Exhibit - Reno, NV, United States
Duration: 5 Jan 20048 Jan 2004

Conference

Conference42nd AIAA Aerospace Sciences Meeting and Exhibit
Country/TerritoryUnited States
CityReno, NV
Period5/01/048/01/04

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