Conjugate Heat Transfer Analysis for High Pressure Cooled Turbine Vane in Aircraft Gas Turbine |
Kim, Jinuk
(Dept. of Mechanical Engineering, Hanyang Univ.)
Bak, Jeonggyu (Dept. of Mechanical Engineering, Hanyang Univ.) Kang, Young-Seok (Engine Component Research Team, Korea Aerospace Research Institute) Cho, Jinsoo (Dept. of Mechanical Engineering, Hanyang Univ.) |
1 | Qiang, W., Zhaoyuan, G., Chi, Z., Guotai, F. and Zhongqi, W., 2009, "Coupled Heat Transfer Simulation of a High-pressure Turbine Nozzle Guide Vane," Chinese Journal of Aeronautics, 22(2009), pp. 230-236. DOI |
2 | Kim, J., Bak, J., Kang, Y., Cho, L. and Cho, J., 2014, "A Study on the Numerical Analysis Methodology for Thermal and Flow Characteristics of High Pressure Turbine in Aircraft Gas Turbine Engine," The KSFM Journal of Fluid Machinery, Vol. 17, No. 3, pp. 46-51. DOI |
3 | Kang, Y. S., Rhee, D. H. and Cha, B. J., 2012, "Aerodynamic design of high pressure turbine for aircraft turbofan engine," Proceeding of the 7th National Congress on Fluids Engineering, pp. 246-247 |
4 | Seo., J. C., Kim., K. W., Hwang., S. W., Son., C. M., Kim., K. S., Rhee., D. H. and Cha., B. J., 2013, "Design of Gas Turbine Engine 1st stage High Pressure Turbine Nozzle Cooling System," Proceedings of the KFMA Annual Meeting, pp. 137-138. |
5 | Song, X., Xie, M., Zhou, F., Jia, G., Hao, X. and An, S., 2011, "High-Temperature Thermal Properties of Yttria Fully Stabilized Zirconia Ceramics," Journal of Rare Earth, Vol. 29, No. 2, pp. 155-159. DOI |
6 | Zhu, D. and Miller, R, A., 1999, "Thermal Conductivity and Elastic Modulus Evolution of Thermal Barrier Coatings Under High Heat Flux Conditions," NASA, TM-1999-209069. |
7 | Reed., R. C., Matan., N., Cox., D. C., Rist, M. A. and Rae., C. M. F., 1999, "Creep of CMSX-4 Superalloy Single Crystals: Effects of Rafting At High Temperature," Acta Materialia, Vol. 47, Issue 12, pp. 3367-3381. DOI |
8 | Tsukamoto, K., Horiuchi, Y., Sugimura, K. and Higuchi, S., 2014, "Conjugate Heat Transfer Analysis in an Actural Gas Turbine Rotor Blade in Comparison with Pyrometer Data," ASME Turbo Expo, GT2014-26962. |
9 | Ho, K. S., Urwiller, C., Konan, S. M., Liu, J. S. and Aguilar, B., 2014, "Conjugate Heat Transfer Analysis for Gas Turbine Cooled Blade," ASME Turbo Expo, GT2014-25952. |
10 | Insinna, M., Griffini, D., Salvadori, S. and Martelli, F., 2014, "Conjugate Heat Transfer Analysis of a Film Cooled High-Pressure Turbine Vane under Realistic Combustor Exit Flow Conditions," ASME Turbo Expo, GT2014-25280. |
11 | Hylton. L. D., Mihelc. M. S., Turner. E. R., Nealy. D. A. and York. R. E., 1983, "Analytical and Experimental Evaluation of The Heat Transfer Distribution over the Surfaces of Turbine Vanes," AAS/Division of Dynamical Astronomy Meeting. |