Experimental Study on Evaporation and Combustion Characteristics of Fuel Droplet with Carbon Nano-particle in RCM

급속압축장치에서 탄소 나노입자가 첨가된 연료 액적의 증발 및 연소 특성에 관한 실험적 연구

  • 안형진 (한국과학기술원 항공우주공학과) ;
  • 원종한 (한국과학기술원 항공우주공학과) ;
  • 백승욱 (한국과학기술원 항공우주공학과) ;
  • 김혜민 (국방과학연구소 7본부 3부)
  • Published : 2015.12.10

Abstract

Evaporation characteristics of a single droplet of carbon nanofluids were investigated in a rapid compression machine(RCM). n-Heptane and carbon black N990 were used to synthesize the carbon nanofluids. RCM is an experimental set-up to simulate a single compression stroke of reciprocating engine. Temperature and pressure in a reaction chamber were measured during the compression stroke. After the piston reaches top dead center(TDC), temperature and pressure decreased due to the heat loss at wall. In that process, a single droplet of carbon nanofluids underwent unsteady condition. A single droplet was put at the center of reaction chamber. Thermocouple whose tip is $50{\mu}m$ was used not only to measure transient bulk temperature, but also to suspend the droplet. The picture of single droplet was taken using high speed camera with a frame rate of 500 fps. From those pictures, the droplet diameter was measured by visual basic program.

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