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Technology / Internal combustion engine / Shchelkin spiral / Pulse detonation engine / Deflagration to detonation transition / Detonation / Fuel injection / Injector / Propane / Jet engines / Combustion / Chemistry


Experimental Study on Deflagration-to-Detonation Transition Enhancement Methods in a PDE T. H. New1, P. K. Panicker2, K. F. Chui3, H. M. Tsai4 and F. K. Lu5
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Document Date: 2006-10-05 02:48:30


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File Size: 616,43 KB

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City

Calgary / Arlington / /

Company

Temasek Laboratories / D. Data / Alternative Fuel Systems Inc. / /

Country

Canada / United Kingdom / Singapore / /

Facility

American Institute / National University of Singapore / Aerospace Engineering Department University of Texas / University of Texas / University of Liverpool / American Institute of Aeronautics / /

IndustryTerm

stainless steel tubes / enhancement device / gas injectors / electronic control systems / low-energy ignition sources / highfrequency high-energy ignition / gas injector / detonation-enhancing devices / solenoid valve gas injectors / non-conventional deflagration-to-detonation transition enhancing devices / high-energy electrical ignition / ignition energy level / gas injector opening / high-strength stainless steel / detonation products / gas injector timing / gas jets / rotary valve systems / similar devices / internal combustion engine gas injectors / measurement systems / higher energy output / gas injector response / gas injectors lies / sufficient energy / propane/oxygen/detonation products / gas injector housing / deflagration-to-detonation transition enhancing devices / high-frequency gas injection / enhancement devices / energy output / larger steel pipes / ignition energy / low-energy ignition / energy limiting / mm diameter hollow metal pipe / stainless steel pipe / /

NaturalFeature

Brownlow Hill / /

Organization

American Institute / University of Texas at Arlington / Aerodynamics Research Centre / Department of Engineering / National University of Singapore / American Institute of Aeronautics / Aerodynamics Research Center / University of Liverpool / American Institute of Aeronautics and Astronautics Fig / /

Person

Kent Ridge Crescent / /

Position

driver / Principal Research Scientist / Lecturer / Scientist / Research Associate / /

ProgrammingLanguage

LabView / /

ProvinceOrState

Texas / /

Technology

ATM / flash / /

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