References
- Suslov, D. I., Arnold, R., and Haidn, O. J., "Convective and Film Cooled Nozzle Extension for a High Pressure Rocket Subscale Combustion Chamber," AIAA-2010-1150, 2010.
- Han, J. C., Dutta, S., and Ekkad, S., Gas Turbine Heat Transfer and Cooling Technology, Taylor & Francis, 1999, pp.1-25.
- http://mpt-llc.com/Patents/tubineairfoil.pdf, "Advances in Turbine Airfoil Cooling Designs Enabled by Improvements in Core Manufacture & Casting Capability".
- Cerri, G., Giovannelli, A., Battisti L., and Fedrizzi, R., "Advances in Effusive Cooling Techniques of Gas Turbines," Applied Thermal Engineering, Vol.27, 2007, pp.692-698. https://doi.org/10.1016/j.applthermaleng.2006.10.012
- Nealy, Davis A., "Combustor Cooling - Old Problems and New Approaches," in Gas Turbine Combustor Design Problems, by Lefebvre, A. H., Hemisphere Publishing Corp., 1980, pp.151-185.
- Brown, S. F. "21st Century Hot Jet Engines," Popular Science, Vol.236, No.6, 1990, pp.83-89.
- Lefebvre, A. H., Gas Turbine Combustion, 2nd Ed., Taylor & Francis, 1999, pp.275-310.
- Wadia, A. R., "Advanced Combustor Liner Cooling Technology for Gas Turbine," Defense Science Journal, Vol.38, No.4, 1988, pp.363-380. https://doi.org/10.14429/dsj.38.5870
- Allison Engine Company and General Motors Corporation, (Latest Owner: Rolls-Royce Corporation, Indianapolis, IN 46241), Sheet Metal (Lamilloy), Registration No. 0889623, 1970.
- http://www.domain-b.com/aero/mil_avi/ miss_muni/20090112_supersonic_cruise_missile.h tml, Aviation & Aerospace News, "Rolls-Royce Completes Initial Test of Engine for Supersonic Cruise Missile Programme (2009.1.12)".
- http://www.euroairport.com
- Clifford, R. J., "Rotating Heat Transfer Investigations on a Multipass Cooling Geometry," AGARD-CP-390, 1985.
- 吉田豊明: 冷却技術, 日本ガスタービン学会誌, 25-97, 1997, pp.29-34.
- Younossi, O., Arena, M. V., Moore, R. M., Lorell, M., Mason, J., and Graser, J. C., "Military Jet Engine Acquisition : Technology Basics and Cost-Estimating Methodology," RAND, MR-1596-AF, 2002.
- 129Langston, L. S., "Fahrenheit 3600, Everywhere You Look, the Great Turbine Industry is Running Hot," Mechanical Engineering (The Magazine of ASME), Vol.129, No.4, 2007, pp.34-37.
- Ruffles, P. C., "Aero Engines of the Future," The Aeronautical Journal, 2003, pp.307- 321.
- Wear, J. D., Trout, A. M., Smith, J. M., and Jones, R. E., "Design and Preliminary Results of a Semi-Transpiration Cooled (Lamilloy) Liner for a High-Pressure, High- Temperature Combustor," AIAA-78-997, 1978.
- Wear, J. D., Trout, A. M. and Smith, J. M., "Performance of Semi-Transpiration-Cooled Liner in High-Temperature-Rise Combustor," NASA-TP-1806, 1981.
- Essman, D. J., Vogel, R. E., Tomlinson, J. G., and Novick, A. S., "TF41/Lamilloy Accelerated Mission Test," AIAA-81-1349, 1981.
-
Auyeung, T. P., Cohn, R., Coy, E., Danczyk, S. A., Papesh, C., and Sweeney, P., "Experimental and Numerical Analysis of Transpiration Cooling of a Rocket Engine Using Lamilloy
${\circledR}$ Plates (POSTPRINT)," AFRLPR- ED-TP-2005-450 (ADA 445014), 2005. - Serbest, E., Haidn, O., Hald, H., Korger, G., and Winkelmann, P., "Effusion Cooling in Rocket Combustors Applying Fiber Reinforced ceramics," AIAA-99-2911, 1999.
- Greuel, D., Herbertz, A., Haidn, O. J., Ortelt, M., and Hald, H., "Transpiration Cooling Applied to C/C Liners of Cryogenic Liquid Rocket Engines," AIAA-2004-3682, 2004.
- Hald, H., Ortelt, M., Fischer, I., Greuel, D., and Haidn, O. J., "Effusion Cooled CMC Rocket Combustion Chamber," AIAA-2005-3229, 2005.
- Steel, S., "Ceramic Materials for Reusable Liquid Fueled Rocket Engine Combustion Devices," The AMPTIAC Quarterly, Vol.8, No.1, 2004. pp.39-43.
- Sozen, M. and Davis, P. A., "Transpiration Cooling of a Liquid Rocket Thrust Chamber Wall, AIAA-2008-4559, 2008.
- Kelly, H. N. and Blosser, M. L., "Active Cooling from the Sixties to NASP," NASA-TM -109079 (N93-12458), 1994.
- Glass, D. E., "Ceramic Matric Composite (CMC) Thermal Protection Systems (TPS) and Hot Structures for Hypersonic Vehicles," AIAA- 2008-2682, 2008.
- 김중연, 박선희, 전병희, 김성현, 정병훈, 한정식, "흡열연료를 이용한 고속비행체 냉각기술 동향," 한국추진공학회지, 제14권, 제2호, 2010, pp.71-79.
- Bouchez, M., Dufour E., and Daniau, E., "Semi-Empirical and CFD Analysis of Actively Cooled Dual-Mode Ramjets: 2006 Status," AIAA -2006-9073, 2006.
- Huang, H., Sobel, D. R., and Spadaccini, L. J., "Endothermic Heat-Sink of Hydrocarbon Fuels for Scramjet Cooling," AIAA-2002-3871, 2002.
- Song, K. D., Choi, S. H., and Scotti, S. J., "Transpiration Cooling Experiment for Scramjet Engine Combustion Chamber by High Heat Fluxes", Journal of propulsion and Power, Vol.22, No.1, 2006, pp.96-102. https://doi.org/10.2514/1.11300
- Gascoin, N., Gillard, P., Dufour, E., and Touré, Y., "Validation of Transient Cooling Modeling for Hypersonic Application, Journal of Thermophysics and Heat Transfer, Vol.21, No.1, 2007, pp.86-94. https://doi.org/10.2514/1.26022
- T. Langener, J. V. Wolfersdorf, M. Kuhn, and J. Steelant, "Transpiration Cooling with Supersonic Flows and Foreign Gas Injection," AIAA-2010-6794, 2010.
- Bennelt, A. I. and McPherson, D. J., "Materials for Large Land-Based Gas Turbines," NMAB-430, 1986,
- 김영길, 홍순형, 백경욱 "초내열 ODS MA 합금 설계 및 응용(제3차년도 최종보고서)," 과학기술처, 1995.
- Nealy, D. A. and Reider, S.B., "Evaluation of Laminated Porous Wall Materials for Combustor Liner Cooling," ASME Paper 79-GT -100, 1979.
- http://www.ultramet.com/propulsionsystem_components_liquid_rocket,html.
- 우상국, 한인섭, "에너지용 다공질 소재의 동향 및 전망," 세라미스트, 제10권, 제6호, 2007, pp.22-30.
- 엄정해, 채수호, 김영욱, "반응소결에 의한 다공질 세라믹스의 제조공정," 세라미스트, 제10 권, 제6호, 2007, pp.14-21.
- 전의진, 이우일, 윤광준, 김태욱, "최신 복합재료," (주)교학사, 1995.
- Bouchez, M. and Beyer, S., "PTAHSOCAR Fuel-Cooled Composite Materials Structure," AIAA-2008-2626, 2008.
- Serbest, E., Haidn, O. J., Greuel, D., Hald, H., and Korger, G., "Effusion Cooling of Throat Region in Rocket Engines Applying Fiber Reinforced Ceramics," AIAA-2001-3410, 2001.
- Ortelt, M., Herbertz, A., and Hald, H., "Investigation on Fiber Reinforced Combustion Chamber Structures under Effusion Cooled LOX/LH2 Operation," AIAA-2009-5475, 2009.
- 김광수, "첨단 탄소 복합재료의 개발 및 응용에 관한 고찰," 요업기술, 제12권, 제2호, 1997, pp.91-100.
- 김옥희, 이승윤, 윤병일, 박종욱, "다층코팅을 이용한 C/C 복합재료의 내산화성 및 내마모성 증진," 한국세라믹학회지, 제32권, 제9호, 1995, pp.1003-1008.
Cited by
- Design and Analysis of Test Facility for the Experiment of Transpiration Cooling in Hot-flow Condition vol.17, pp.2, 2013, https://doi.org/10.6108/KSPE.2013.17.2.046