1987
DOI: 10.2514/3.22986
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Effects of alternative fuels on ignition limits of the J85 annular combustor

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1987
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Cited by 8 publications
(2 citation statements)
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“…Previous gas turbine ignition investigations [27,28] aimed to improve the ignition performance of a particular combustor by examining the ignitability of different flow conditions or different spark parameters. The spark location, for instance, is probably influenced more by accessibility and replacement considerations and not based on any analysis of the mixing pattern and the velocity field.…”
Section: Introductionmentioning
confidence: 99%
“…Previous gas turbine ignition investigations [27,28] aimed to improve the ignition performance of a particular combustor by examining the ignitability of different flow conditions or different spark parameters. The spark location, for instance, is probably influenced more by accessibility and replacement considerations and not based on any analysis of the mixing pattern and the velocity field.…”
Section: Introductionmentioning
confidence: 99%
“…GE-J85 engine (a turbojet engine) was selected for this study because of the widely used area (for high performance trainers and tactical aircraft), high experience rate (more than 75 million flight hours experience on military and commercial models), having too many aircraft engines (more than 6000 engines have been flying in a number of applications remain in active service in 35 countries since 1960), previous environmental studies (such as noise [59]), and alternative fueled production [60,61]. Current plans for the U.S. Air Force (USAF) call for J85-powered aircrafts to be in service through 2040 [62].…”
Section: Description Of Aircraft Enginesmentioning
confidence: 99%