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AviationTest Facilities, Equipment and Methods

Effects of Corona, Spark and Surface Discharges on Ignition Delay and Deflagration-to-Detonation Times in Pulsed Detonation Engines (Postprint)

Authors: Kenneth Busby; Jennifer Corrigan; Sheng-Tao Yu; Skip Williams; Campbell Carter; Frederick Schauer; John Hoke; Charles Cathey; Martin Gundersen; AIR FORCE RESEARCH LAB WRIGHT-PATTERSON AFB OH PROPULSION DIRECTORATE
 
Abstract: The purpose of the research described herein is to compare the ignition delays in an experimental pulsed detonation engine produced by thermal and non-thermal ignitions. The commercial thermal ignition has a pulse duration of about 1 microsec, whereas the non-thermal ignitions have pulse durations of 100 nanosec. Ignition delay is an important factor, along with fill and purge times, that limit the maximum repetition rate and thrust of pulsed detonation engines. For stoichiometric fuel-air mixtures with aviation gasoline at 1 atmosphere and 360 - 480 K, an ignition delay of 6 millisec was observed with a non-thermal ignition, whereas the ignition delay was 11 millisec with an aftermarket automotive ignition. By replacing the resistive cable and resistor of the aftermarket ignition with a non-resistive cable and surface discharge igniter, its ignition delay was reduced to 7 millisec, which is comparable to that produced by the non-thermal ignitions.

Limitations: APPROVED FOR PUBLIC RELEASE
Description: Conference paper
Pages: 12
Report Date: DEC 2006
Contract Number: F4962002C0015
Report Number: A426874
Keywords relating to this report:
*IGNITION LAG
*IGNITION SYSTEMS
AVIATION GASOLINE
DETONATION WAVES
EXPERIMENTAL DESIGN
IGNITERS
INSTRUMENTATION
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