Acknowledgement
본 연구는 (주)LIG넥스원(63985-01)의 지원으로 수행되었으며, 지원에 감사드립니다.
References
- Bennett, C.O. and Myers, J.E., "Momentum, Heat, and Mass Transfer," 3rd edition, McGRAW-HILL, New York, N.Y., U.S.A, 1983.
- Colburn, A.P., "A method of correlating forced convection heat-transfer data and a comparison with fluid friction," International Journal of Heat and Mass Transfer, Vol. 7, No. 12, pp. 1359-1384, 1964. https://doi.org/10.1016/0017-9310(64)90125-5
- Bartz, D.R., "A simple equation for rapid estimation of rocket nozzle convective heat transfer coefficients," Jet Propulsion, Vol. 27, No. 1, pp. 49-51, 1957. https://doi.org/10.2514/8.12572
- Bartz, D.R., "Turbulent Boundary-Layer Heat Transfer from Rapidly Acceleration Flow of Rocket Combustion Gases and of Heated Air," Advances in Heat Transfer, Vol. 2, pp. 2-108, 1965.
- Betti, "Flow Field and Heat Transfer Analysis of Oxygen/Methane Liquid Rocket Engine Thrust Chambers," Ph.D. Thesis, Department of Mechanical and Aerospace Engineering, Sapienza University of Rome, Rome, Italy, 2012.
- Schuff, R., Maier, M., Sindiy, O., Ulrich, C. and Fugger, S., "Integrated Modeling and Analysis for a LOX/Methane Expander Cycle Engine: Focusing on Regenerative Cooling Jacket Design," 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Sacramento, C.A., U.S.A., AIAA 2006-4534, Jul. 1957.
- Nichols, R.H. and Nelson, C.C., "Wall Function Boundary Conditions Including Heat Transfer and Compressibility," AIAA Journal, Vol. 42, No. 6, pp. 1107-1114, June 2004. https://doi.org/10.2514/1.3539
- Bensayah, K., Hadjadj, A. and Bounif, A., "Heat Transfer in Turbulent Boundary Layers of Conical and Bell Shaped Rocket Nozzles with Complex Wall Temperature, Numerical Heat Transfer," Part A: Applications: An International Journal of Computation and Methodology, Vol. 66, No. 3, pp. 289-314, May 2014. https://doi.org/10.1080/10407782.2013.873283
- Hahm, H.C. and Kang, Y.G., "Comparative Studies of Heat Transfer Coefficients for Rocket Nozzle," Journal of the Korean Society of Propulsion Engineers, Vol. 16, No. 2, pp. 42-50, Apr. 2012. https://doi.org/10.6108/KSPE.2012.16.2.042
- Back, L.H., Massier, P.F. and Gier, H.L, "Convective heat transfer in a convergent-divergent nozzle," International Journal of Heat and Mass Transfer, Vol. 7, No. 5, pp. 549-568, May 1964. https://doi.org/10.1016/0017-9310(64)90052-3
- Kim, Y.G., Bae, J.C. and Kim, J.O., "Parametric comparative study of Rocket Nozzle Convective Heat Transfer Coefficient Application of Combustion gas characteristic and Method of Analysis," 48th KSPE Spring Conference, Jeju, Korea, pp. 651-663, May 2017.
- Huzel, D.K. and Huang, D.H., Modern engineering for design of liquid-propellant rocket engines, 1st ed, American Institute of Aeronautics and Astronautics, U.S.A., 1992.
- Pavli, A.J., Curley, J.K., Masters, P.A. and Schwartz, R.M., "Design and Cooling Performance of A Dump-Cooled Rocket Engine," NASA TN-D-3532, 1966.
- Simcenter STAR-CCM+ 2019.1,"Simcenter STAR-CCM+® Documentation Version 2019.1," Siemens, Wittelsbacherpl. 1, 80333 Munchen, Germany, 2019.
- Kader, B.A, "Temperature and concentration profiles in fully turbulent boundary layers," International Journal of Heat and Mass Transfer, Vol. 24, No. 9, pp. 1541-1544, 1981. https://doi.org/10.1016/0017-9310(81)90220-9
- Kam, H.D, Kim, J.S., "Assessment and Validation of Turbulence Models for the Optimal Computation of Supersonic Nozzle Flow," Journal of the Korean Society of Propulsion Engineers, Vol. 17, No. 1, pp. 18-25, 2013. https://doi.org/10.6108/KSPE.2013.17.1.018