Effective Modeling of Conjugate Heat Transfer and Hydraulics for the Regenerative Cooling Design of Kerosene Rocket Engines

REFERENCES

• D. K. Huzel and D. H. Huang , Modern Engineering for Design of Liquid-Propellant Rocket Engines , AIAA , Washington , DC , 1992 .
   Google Scholar
• G. P. Sutton , History of Liquid Propellant Rocket Engines , AIAA , Reston , VA , 2005.
   Google Scholar
• Y. Daimon , H. Negishi , N. Yamanishi , Y. Nunome , M. Sasaki , and T. Tomita , Combustion and Heat Transfer Modeling in Regeneratively Cooled Thrust Chambers, 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, AIAA 2012-4009, Atlanta, Georgia , 2012 .
   Google Scholar
• F. Zhong , X. Fan , G. Yu , J. Li , and C.-J. Sung , Heat Transfer of Aviation Kerosene at Supercritical Conditions , Journal of Thermophysics and Heat Transfer , vol. 23 , pp. 543 – 550 , 2009 .
   Web of Science ®Google Scholar
• M. H. Naraghi , S. Dunn , and D. Coats , A Model for Design and Analysis of Regeneratively Cooled Rocket Engines, 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, AIAA 2004-3852, Fort Lauderdale, FL , 2004 .
   Google Scholar
• J. Jokhakar and M. H. Naraghi , A CFD-RTE Model for Thermal Analysis of Regeneratively Cooled Rocket Engines, 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA-2008-4557, Hartford, CT , 2008 .
   Google Scholar
• J. Görgen , T. Aichner , and M. Frey , Spray Combustion and Heat Transfer Modeling in LOx/H2, LOx/HC and MMH/NTO Combustion Chamber, 3th European Conference for Aerospace Sciences, EUCASS 2009-104, Versailles, France , 2009 .
   Google Scholar
• O. Knab , M. Frey , J. Görgen , C. Maeding , K. Quering , and D. Wiedmann , Progress in Combustion and Heat Transfer Modelling in Rocket Thrust Chamber Applied Engineering, 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, AIAA 2009-5477, Denver, Colorado , 2009 .
   Google Scholar
• D. Preclik , O. Knab , J. Görgen , and G. Hagemann , Simulation and Analysis of Thrust Chamber Flowfields: Cryogenic Propellant Rockets , in V. Yang , M. Habiballah , J. Hulka , and M. Popp (eds.), Liquid Rocket Thrust Chambers: Aspects of Modeling, Analysis and Design , chap. 15 , AIAA , Reston , VA , pp. 527 – 551 , 2004 .
   Google Scholar
• H. W. Zhang , Y. L. He , and W. Q. Tao , Numerical Study of Film and Regenerative Cooling in a Thrust Chamber at High Pressure , Numerical Heat Transfer, Part A , vol. 52 , pp. 991 – 1007 , 2007 .
   Web of Science ®Google Scholar
• M. Pizzarelli , S. Carapellese , and F. Nasuti , A Quasi-2-D Model for the Prediction of the Wall Temperature of Rocket Engine Cooling Channels , Numerical Heat Transfer, Part A , vol. 60 , pp. 1 – 24 , 2011 .
   Web of Science ®Google Scholar
• M. Pizzarelli , F. Nasuti , and M. Onofri , Analysis of Curved-Cooling-Channel Flow and Heat Transfer in Rocket Engines , Journal of Propulsion and Power , vol. 27 , pp. 1045 – 1053 , 2011 .
   Web of Science ®Google Scholar
• T. S. Park , Effects of Aspect Ratio on the Turbulent Heat Transfer of Regenerative Cooling Passage in a Liquid Rocket Engine , Numerical Heat Transfer, Part A , vol. 64 , pp. 710 – 728 , 2013 .
   Web of Science ®Google Scholar
• Y.-D. Kang and B. Sun , Numerical Simulation of Liquid Rocket Engine Thrust Chamber Regenerative Cooling , Journal of Thermophysics and Heat Transfer , vol. 25 , pp. 155 – 164 , 2011 .
   Web of Science ®Google Scholar
• H. Negishi , Y. Daimon , H. Kawashima , and N. Yamanishi , Flowfield and Heat Transfer Characteristics of Cooling Channel Flows in a Methane-Cooled Thrust Chamber, 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, AIAA 2012–4122, Atlanta, Georgia , 2012 .
   Google Scholar
• S.-K. Kim , M. Joh , H. S. Choi , and T. S. Park , Multidisciplinary Simulation of a Regeneratively Cooled Thrust Chamber of Liquid Rocket Engine: Turbulent Combustion and Nozzle Flow , International Journal of Heat and Mass Transfer , vol. 70 , pp. 1066 – 1077 , 2014 .
   Web of Science ®Google Scholar
• H. S. Choi , Y.-M. Han , Y.-M. Kim , and G.-R. Cho , Development of 30-ton f LOx/Kerosene Rocket Engine Combustion Devices(I) – Combustion Chamber , Journal of The Korean Society for Aeronautical and Space Sciences (in Korean) , vol. 37 , pp. 1027 – 1037 , 2009 .
   Google Scholar
• M. B. Dobrovolskij , Liquid Rocket Engines: Basic Design, , 2nd ed. (in Russian), ISBN 5-7038-2649-7, MGTU imeni N.E. Baumana, 2006.
   Google Scholar
• I. E. Idelchik , Handbook of Hydraulic Resistance, , 3rd ed. , Begell House , New York , 1996 .
   Google Scholar
• T. J. Bruno and M. L. Huber , Evaluation of the Physicochemical Authenticity of Aviation Kerosene Surrogate Mixtures. Part 2: Analysis and Prediction of Thermophysical Properties , Energy & Fuels , vol. 24 , pp. 4277 – 4284 , 2010 .
   Web of Science ®Google Scholar
• M. L. Huber , NIST Thermophysics Properties of Hydrocarbon Mixtures Database (SUPERTRAPP), Version 3.1 User's Guide , U.S. Department of Commerce , Gaithersburg , MD , 2003 .
   Google Scholar
• M. L. Huber and H. J. M. Hanley , The Corresponding-States Principle: Dense Fluids , in J. Millat , J. H. Dymond , and C. A. Nieto de Castro (eds.), Transport Properties of Fluids , pp. 283 – 295 , Cambridge University Press , 1996 .
   Google Scholar
• N. Carlson and B. L. Stoner , Thermal Barrier Coating on High Temperature Industrial Gas Turbine Engines , NASA CR-135147 , February , 1977 .
   Google Scholar
• M. Pizzarelli , A. Urbano , and F. Nasuti , Numerical Analysis of Deterioration in Heat Transfer to Near-Critical Rocket Propellants , Numerical Heat Transfer, Part A , vol. 57 , pp. 297 – 314 , 2010 .
   Web of Science ®Google Scholar
• Color versions of one or more of the figures in the article can be found online at www.tandfonline.com/unht.
   Google Scholar