舰船科学技术
艦船科學技術
함선과학기술
SHIP SCIENCE AND TECHNOLOGY
2014年
10期
55-58,72
,共5页
胡广%胡刚义%唐滢%彭学创
鬍廣%鬍剛義%唐瀅%彭學創
호엄%호강의%당형%팽학창
微通道%可压缩性%提前转捩%进口段%沿程阻力%数值仿真
微通道%可壓縮性%提前轉捩%進口段%沿程阻力%數值倣真
미통도%가압축성%제전전렬%진구단%연정조력%수치방진
microchannels%compressibility%transition forward%entrance length%numerical analysis
对空气在当量直径0.5 mm和1.0 mm微通道中的流动特性进行数值仿真研究与分析。分析结果表明,微通道在平均马赫数0.15左右就必须考虑可压缩性影响。微通道在Re为1380左右即发生提前转捩现象,提前转捩和可压缩性都将使沿程阻力增加。微通道受进口段影响,压强降较大,但微通道层流进口段长度和湍流进口段长度均小于常规通道。
對空氣在噹量直徑0.5 mm和1.0 mm微通道中的流動特性進行數值倣真研究與分析。分析結果錶明,微通道在平均馬赫數0.15左右就必鬚攷慮可壓縮性影響。微通道在Re為1380左右即髮生提前轉捩現象,提前轉捩和可壓縮性都將使沿程阻力增加。微通道受進口段影響,壓彊降較大,但微通道層流進口段長度和湍流進口段長度均小于常規通道。
대공기재당량직경0.5 mm화1.0 mm미통도중적류동특성진행수치방진연구여분석。분석결과표명,미통도재평균마혁수0.15좌우취필수고필가압축성영향。미통도재Re위1380좌우즉발생제전전렬현상,제전전렬화가압축성도장사연정조력증가。미통도수진구단영향,압강강교대,단미통도층류진구단장도화단류진구단장도균소우상규통도。
Numerical experiments are conducted for gaseous flow though microchannels with hydraulic diameter de =0. 5 mm and 1. 0 mm. The experiments results show that compressibility increase significantly when mean Ma is above 0. 15. The transition Reynolds number is brought forward to about 1 380. For the gaseous flow in the entrance length regime, an evident pressure loss is observed. The entrance length of laminar flow and turbulent flow in microchannels is less than that in conventional channels.