请教kiva问题

forestwoods

kiva是否只能生成气缸形状的计算域，能否用于超燃计算？
谢谢!

chwe

报导号 A9835083
报告号 AIAA Paper 98-3214
语种 English
题名 Effects of fuel-injection parameters in a side-dump ramjet combustor
责任者 Jiang, Tsung L.^Shen, Chih-Hung (National Cheng Kung Univ., Tainan, Taiwan)
机构  
出处 AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 34th, Cleveland, OH, July 13-15, 1998, 12 p..
注释  
出版时间 1998
叙词 AIRCRAFT ENGINES; RAMJET ENGINES; DUMP COMBUSTORS; FUEL INJECTION; COMBUSTIBLE FLOW; JET IMPINGEMENT; FUEL SPRAYS; THREE DIMENSIONAL FLOW; FLOW CHARACTERISTICS; TEMPERATURE PROFILES; COMPUTER PROGRAMS
文摘 The spray-combustion flow of a side-dump ramjet combustor attached symmetrically to four inlets is analyzed numerically by using a modified KIVA-3 computer code. ^Numerical results obtained from the present study reveal that open circulating flows, exhibiting 3D structures, occur in the region between the jet-impingement point and the dome head, and pairing vortices appear in the surroundings of impinging jets. ^Injector positions are found to have strong effects on fuel distributions and flame structures, while effects of injection cant-angles on the flame structure are relatively limited. ^Injectors installed on the inlet-duct wall near the dome are responsible for the fuel distribution in the dome region, since the fuel penetration depth is short under the high-speed air stream in the inlet. ^Those on the opposite wall of inlet ducts, however, dominate the fuel distribution in the downstream region of the combustor. ^The flame structure is closely associated with the fuel distribution and the local stoichiometry. ^(Author)
分类号 7507 Aircraft Propulsion & Power (1975-)|