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Measurements of the blowout limits of supercritical aviation kerosene in a supersonic combustor
Wang J(王晶); Fan XJ(范学军); Zhang TC(张泰昌); Yu G(俞刚); Li JG(李建国); Wang J(王晶)
Source Publication47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011
2011
Conference Name47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011
Conference DateJUL 31-AUG 03, 2011
Conference PlaceSan Diego, CA, United states
AbstractCombustion and flame stability of supercritical kerosene were studied experimentally in a supersonic model combustor at various air and fuel conditions. The lean and rich blowout limits of supercritical kerosene injected from the bottom of a cavity flameholder were examined in Mach 2.5 airflow. It was found that the rich blowout limit was very sensitive to the stagnation temperature of the airflow while the lean limit was only slightly affected. Damkohler number was used to correlate the two limits. On the other hand, the lean blowout limits of supercritical kerosene injected upstream the cavity were investigated and compared at three different Mach numbers of 2.0, 2.5 and 3.0. ? 2011 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
DepartmentLHD超声速燃烧
Funding OrganizationAmerican Institute for Aeronautics and Astronautics (AIAA)
ISBN9781600869495
Indexed ByEI
Language英语
Document Type会议论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/48277
Collection高温气体动力学国家重点实验室
Corresponding AuthorWang J(王晶)
Recommended Citation
GB/T 7714
Wang J,Fan XJ,Zhang TC,et al. Measurements of the blowout limits of supercritical aviation kerosene in a supersonic combustor[C]:AMER INST AERONAUT ASTRONAUT, RESTON,2011.
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