• 검색 결과가 없습니다.

A SPACIAL ANALYSIS OF IN-CYLINDER TURBULENCE FLOW IN SI ENGINE USING CROSS CORRELATION PIV

N/A
N/A
Protected

Academic year: 2021

Share "A SPACIAL ANALYSIS OF IN-CYLINDER TURBULENCE FLOW IN SI ENGINE USING CROSS CORRELATION PIV"

Copied!
6
0
0

로드 중.... (전체 텍스트 보기)

전체 글

(1)

상호상관 PIV기법을 이용한 엔진 실린더내 난류의 공간적 해석

정구섭

정용욱

*

A SPACIAL ANALYSIS OF IN-CYLINDER TURBULENCE FLOW

IN SI ENGINE USING CROSS CORRELATION PIV

Kuseob Chung, Yongoug Chung

Key Words: PIV(입자영상유속계), Cross correlation(상호상관), SCV(스월제어밸브), Velocity

vector(속도벡터)

Abstract

Tumble or swirl flow is used adequately to promote mixing of air and fuel in the cylinder and to enlarge turbulent intensity in the late time of compression stroke. However, since in-cylinder flow is a kind of transient state with rapid flow variation, that is, non-steady state flow, swirl or tumble flow has not been analyzed sufficiently and not been recognized whether they are available for combustion theoretically yet. In the investigation of intake turbulent characteristics using PIV method, different flow characteristics were showed according to SCV figures. SCV installed engine had higher vorticity, turbulent strength by fluctuation and turbulent kinetic energy than a baseline engine, especially around the wall and lower part of the cylinder. Consequently, as swirl flow was added to existing tumble flow, it was found that fluctuation component increased and flow energy was conserved effectively through the experiment.

1. 서 론

(2)

2. 실험장치 및 방법

2.1 실험장치 및 실험조건 μ 2.2 속도벡터계산과 후처리 Blower Laminar flowmeter Manometer Cylinder head Tumble adaptor Laskin nozzle CCD camera Frame grabber Insight NT 1.22 Cylinderical lens Pressurized air Laser pulse synchronizer Laser power supplies

Dual Nd:YAG laser Synchronizer

(3)

3. 실험결과 및 고찰

3.1 엔진 실린더내 유속분포 μ In Ex 0 60 40 20 In Ex 0 60 40 20 In Ex 0 80 60 40 20 0 20 -40 -20 40 In Ex 0 80 60 40 20 0 20 -40 -20 40 In Ex 0 80 60 40 20 0 20 -40 -20 40 In Ex 0 80 60 40 20 0 20 -40 -20 40 In Ex 0 80 60 40 20 0 20 -40 -20 40 In Ex 0 80 60 40 20 0 20 -40 -20 40 In Ex 0 60 40 20 In Ex 0 60 40 20

(4)

3.2 스월조절밸브 부착시 실린더내의 유동특성 3.3 실린더내의 와도(Vorticity)분포 ω ω = 1 2( ∂

v

x

-∂

u

y

)

(5)

3.4 실린더내의 난류강도 분포 0 2 4 6 8 10 0.5 1.0 1.5 2.0 Base SCVA SCVB SCVC urms (m /s ) Valve lift, L(mm) 0 2 4 6 8 10 0.5 1.0 1.5 2.0 Base SCVA SCVB SCVC vrm s (m /s) Valve lift, L(mm) 3.5 실린더내의 에너지소산 분포

(6)

4 3 2 6 6 3 1 1 2 1 1 1 1 1 1 7 3 8 3 5 5 1 1 14 1 7 15 3.33E-03 14 3.10E-03 13 2.88E-03 12 2.66E-03 11 2.44E-03 10 2.22E-03 9 2.00E-03 8 1.77E-03 7 1.55E-03 6 1.33E-03 5 1.11E-03 4 8.87E-04 3 6.65E-04 2 4.44E-04 1 2.22E-04 In Ex 0 80 60 40 20 0 20 -40 -20 40 9 9 14 13 11 12 3 4 7 7 6 7 2 2 3 2 3 8 5 4 7 4 4 9 3 15 1.64E-04 14 1.53E-04 13 1.42E-04 12 1.31E-04 11 1.20E-04 10 1.09E-04 9 9.83E-05 8 8.74E-05 7 7.65E-05 6 6.56E-05 5 5.47E-05 4 4.38E-05 3 3.29E-05 2 2.20E-05 1 1.11E-05 In Ex 0 80 60 40 20 0 20 -40 -20 40 15 1.41E-04 14 1.32E-04 13 1.22E-04 12 1.13E-04 11 1.03E-04 10 9.40E-05 9 8.46E-05 8 7.52E-05 7 6.59E-05 6 5.65E-05 5 4.71E-05 4 3.77E-05 3 2.83E-05 2 1.89E-05 1 9.51E-06 13 11 5 2 12 7 4 4 9 6 6 5 6 6 6 2 1 2 1 2 3 4 3 4 4 2 3 3 In Ex 0 80 60 40 20 0 20 -40 -20 40 11 3 1 5 5 1 6 5 6 4 5 6 6 3 3 4 4 3 2 1 2 2 4 3 3 2 3 3 1 5 15 1.51E-04 14 1.41E-04 13 1.31E-04 12 1.21E-04 11 1.11E-04 10 1.01E-04 9 9.06E-05 8 8.06E-05 7 7.05E-05 6 6.05E-05 5 5.04E-05 4 4.03E-05 3 3.03E-05 2 2.02E-05 1 1.01E-05 In Ex 0 80 60 40 20 0 20 -40 -20 40 0 2 4 6 8 1 0 0.0 2.0x10-5 4.0x10-5 6.0x10-5 8.0x10-5 1.0x10-4 B ase S C V A S C V B S C V C D issi p a ti on en er g y ( W /k g) V alve lift, L (m m )

4. 결 론

참고문헌

󰡒

참조

관련 문서

Using selected engine performance simulation results as input to the intake faces of the nozzles and ejector CFD simulation to determine pressure loss, temperature levels and

This work builds inversely a base performance model of a turboprop engine to be used for a high altitude operation UAV using measured performance data,

 A series of systems for configuring alarm and control functions by monitoring the states of main engine, generator, and auxiliary equipment, for securing the safety

→ For the turbulent jet motion and heat and mass transport, simulation of turbulence is important.. in the mean-flow equations in a way which close these equations by

1) Derive shear flow dispersion equation using Taylor’ analysis (1953, 1954) - laminar flow in pipe (1953).. -

7.2 Turbulent Flow and Eddy Viscosity 7.3 Fluid Flow Past Solid Boundaries 7.4 Characteristics of Boundary Layers 7.5 The Laminar Boundary Layer*.. 7.6 The

7.2 Turbulent Flow and Eddy Viscosity 7.3 Fluid Flow Past Solid Boundaries 7.4 Characteristics of Boundary Layers 7.5 The Laminar Boundary Layer*.. 7.6 The

~ depends on the relative importance of the turbulent transport terms For the turbulent jet motion, simulation of turbulence is important. For the horizontal motion in