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Cites:

Information Journal Paper

Title

TRANSIENT SIMULATION OF A SI ENGINE PISTON TEMPERATURE, USING COMBUSTION CHAMBER THERMAL ANALYSIS AND RESISTOR-CAPACITOR METHOD

Pages

  71-84

Abstract

 In this study, the SI engine PISTON heat transfer is calculated. In order to simulate the combustion chamber heat transfer and the transient temperature of the PISTON, a resistor-capacitor model for wall temperature prediction is used. Twenty four heat transfer equations coupled with two-zonal combustion model were solved simultaneously, based on the RESISTOR-CAPACITOR THERMAL NETWORK model. The model predicts the wall temperature well. For each model parameter, an expression as a function of the engine geometry, operational parameters, and material properties were derived to make the model applicable to other similar engines. The simulations were performed writing a computer program on MATLAB and the results were validated using the experimental data of the EF7.TC engine.

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    Cite

    APA: Copy

    GHARLOGHY, J., & KAKAEE, A.H.. (2010). TRANSIENT SIMULATION OF A SI ENGINE PISTON TEMPERATURE, USING COMBUSTION CHAMBER THERMAL ANALYSIS AND RESISTOR-CAPACITOR METHOD. AEROSPACE MECHANICS JOURNAL, 6(2 (20)), 71-84. SID. https://sid.ir/paper/102002/en

    Vancouver: Copy

    GHARLOGHY J., KAKAEE A.H.. TRANSIENT SIMULATION OF A SI ENGINE PISTON TEMPERATURE, USING COMBUSTION CHAMBER THERMAL ANALYSIS AND RESISTOR-CAPACITOR METHOD. AEROSPACE MECHANICS JOURNAL[Internet]. 2010;6(2 (20)):71-84. Available from: https://sid.ir/paper/102002/en

    IEEE: Copy

    J. GHARLOGHY, and A.H. KAKAEE, “TRANSIENT SIMULATION OF A SI ENGINE PISTON TEMPERATURE, USING COMBUSTION CHAMBER THERMAL ANALYSIS AND RESISTOR-CAPACITOR METHOD,” AEROSPACE MECHANICS JOURNAL, vol. 6, no. 2 (20), pp. 71–84, 2010, [Online]. Available: https://sid.ir/paper/102002/en

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