• 제목/요약/키워드: Coaxial Swirling Stream

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노즐 형상이 부족팽창 동축제트 근접 유동장에 미치는 영향 (Effect of Nozzle Geometry on the Near Field Structure of Under Expanded, Dual, Coaxial Jet)

  • 이권희;세토구치토시아키;김희동
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2004년도 춘계학술대회
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    • pp.1649-1654
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    • 2004
  • The near field structures of an under-expanded, dual, coaxial, jets issuing from the coaxial nozzles with four different geometries are visualized by using a shadowgraph optical method. Experiments are conducted to investigate the effects of the nozzle-lip thickness, secondary stream thickness, the nozzle pressure ratio and the secondary swirl stream on the characteristics of under-expanded jets. The results show that the presence of secondary annular swirling stream causes the Mach disk to move further downstream and increases its diameter, which decreases with a decrease in the nozzle-lip thickness. The secondary stream thickness has an influence on the location of an annular shock wave.

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환형 유동을 수반하는 초음속 스월 제트 유동의 가시화 (Visualization of the Supersonic Swirl Jet with Annular Stream)

  • 김중배;이권희;;김희동
    • 한국가시화정보학회:학술대회논문집
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    • 한국가시화정보학회 2003년도 추계학술대회 논문집
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    • pp.91-94
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    • 2003
  • The present study addresses experimental results to investigate the details of the near field flow structures produced in the under-expanded, dual, coaxial, swirling, jet. The sonic swilling jets are emitted from a sonic inner nozzle and the outer annular nozzle produces the co/counter swirling streams against the primary swirling jet, respectively. The interactions between both the secondary annular swirling and primary inner supersonic swirling jets are quantified by the pilot impact and static pressure measurements, and visualized by using the Schlieren optical method. The experiment has been performed fur different swirl intensities and pressure ratios. The results obtained show that the secondary co-swirling jet significantly changes the inner under-expanded swirling jet, such as the recirculation zone, pressure distribution, through strong interactions between both the swirling jets, and the effect of the secondary counter-swirling jet on the primary inner jet is similar to the secondary co-swirl jet case.

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동축의 선회류들이 배합되는 연소기내 난류유동의 수치해석 (Computation of Turbulent Flows in Swirl Combustor)

  • 백석철;김광용
    • 대한기계학회논문집
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    • 제10권4호
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    • pp.511-518
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    • 1986
  • 본 연구에서는 난류모델로는 기존의 K-.epsilon.모델과 LPS방법으로 수정된 K-.epsilon. 모 델을, 수치적 Scheme으로는 Hybrid Difference Scheme과 Skew-upwind Difference Sc- heme을 사용하여 그 결과를 각각 비교하였다.