Numerical Evaluation of Heat Transfer Enhancement in Rocket Thrust Chambers by Wall Ribs

REFERENCES

• R. C. Parsley , B. Zhang , V. Yang , M. Habiballah , M. Popp , and J. Hulka , Thermodynamic Power Cycles for Pump-fed Liquid Rocket Engines , Liquid Rocket Thrust Chambers: Aspects of Modeling, Analysis, and Design , pp. 621 – 648 , 1995 .
   Google Scholar
• R. Pugh , The Many Facets of the rl-10 Liquid Rocket Engine, a Continuing Success Story, 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, July 13–15, 1998, Cleveland, OH, AIAA-98-3680 .
   Google Scholar
• S. Peery and A. Minick , Design and Development of an Advanced Expander Combustor, 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, July 13–15, 1998, Cleveland, OH, AIAA-98-3675 .
   Google Scholar
• V. Rachuk and N. Titkov , The First Russian lox-lh2 Expander Cycle lre: Rd0146, 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, July 9–12, 2006, Sacramento, CA, AIAA-2006-4904 .
   Google Scholar
• M. Fujita , H. Aoki , T. Nakagawa , T. Tokunaga , M. Yasui , and K. Iwama , Upper Stage Propulsion System for h-iia Launch Vehicle, 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, July 7–10, 2002, Indianapolis, IN, AIAA-2002-4212 .
   Google Scholar
• O. Knab , A. Frohlich , D. Wennerberg , and W. Haslinger , Advanced Cooling Circuit Layout for the Vinci Expander Cycle Thrust Chamber, 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 7–10, July, 2002, Indianapolis, IN, AIAA-2002-4005 .
   Google Scholar
• P. Caisso , A. Souchier , C. Rothmund , P. Alliot , C. Bonhomme , W. Zinner , R. Parsley , T. Neill , S. Forde , R. Starke , W. Wang , M. Takahashi , M. Atsumi , and D. Valentian , A Liquid Propulsion Panorama , Acta Astronautica , vol. 65 , pp. 1723 – 1737 , 2009 .
   Web of Science ®Google Scholar
• H. Immich , J. Alting , J. Kretschmer , and D. Preclik , Technology Developments for Thrust Chambers of Future Launch Vehicle Liquid Rocket Engines , Acta Astronautica , vol. 53 , pp. 597 – 605 , 2003 .
   Web of Science ®Google Scholar
• R. D. Baily , Enhanced Heat Transfer Combustor Technology, Subtasks 1 and 2, Tast c.1 , Tech. Rep. NASA-CR-179541, NASA , 1986 .
   Google Scholar
• H. Kawashima , H. Sakamoto , M. Takahashi , M. Sasaki , and A. Kumakawa , Hot-Gas-Side Heat Transfer Characteristics of a Ribbed Combustor, 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, August 2–5, 2009, Denver, CO, AIAA-2009-5476 .
   Google Scholar
• H. Negishi , A. Kumakawa , S. Moriya , N. Yamanishi , and H. Sunakawa , Numerical Investigations of Heat Transfer Enhancement in a Thrust Chamber with Hot Gas Side Wall Ribs, 47th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition, 5–8 January 2009, Orlando, FL, AIAA-2009-830 .
   Google Scholar
• K.-S. Choi , Near-Wall Structure of a Turbulent Boundary Layer with Riblets, J. of Fluid Mechanics , vol. 208, pp. 417–458, 1989.
   Web of Science ®Google Scholar
• B. E. Launder and S. P. Li , On the Prediction of Riblet Performance with Engineering Turbulence Models , Appl. Scientific Research , vol. 50 , pp. 283 – 298 , 1993 .
   Google Scholar
• M. K. Jensen and A. Vlakancic , Technical Note Experimental Investigation of Turbulent Heat Transfer and Fluid Flow in Internally Finned Tubes , Int. J. of Heat and Mass Transfer , vol. 42 , pp. 1343 – 1351 , 1999 .
   Web of Science ®Google Scholar
• J.-H. Kim , K. E. Jansen , and M. K. Jensen , Analysis of Heat Transfer Characteristics in Internally Finned Tubes , Numer. Heat Transfer A , vol. 46 , pp. 1 – 21 , 2004 .
   Web of Science ®Google Scholar
• P. Spalart and S. Allmaras , A One-Equation Turbulence Model for Aerodynamic Flows , La Recherche Aerospatiale , vol. 1 , pp. 5 – 23 , 1994 .
   Google Scholar
• A. Harten , B. Engquist , S. Osher , and S. R. Chakravarthy , Uniformly High Order Accurate Essentially Non-Oscillatory Schemes, III , J. Comput. Phys. , vol. 131 , pp. 3 – 47 , 1997 .
   Web of Science ®Google Scholar
• P. Cinnella , Flux-Split Algorithms for Flows with Non-Equilibrium Chemistry and Thermodynamics, Ph.D. thesis, Virginia Polytechnic Inst. and State Univ., Blackburg , 1989 .
   Google Scholar
• M. Pizzarelli , F. Nasuti , R. Paciorri , and M. Onofri , Numerical Analysis of Three-Dimensional Flow of Supercritical Fluid in Cooling Channels , AIAA J. , vol. 47 , pp. 2534 – 254 , 2009 .
   Google Scholar
• B. Betti , Flow Field and Heat Transfer Analysis of Oxygen/Methane Liquid Rocket Engine Thrust Chambers, Ph.D. thesis, Sapienza University of Rome, Rome, Italy , 2012 .
   Google Scholar
• J. H. Leinard IV , and J. H. Leinard V , A Heat Transfer Textbook , Phlogiston Press , Lexington , MA , 2005 .
   Google Scholar
• R. Schuff , M. Maier , O. Sindiy , C. Ulrich , and S. Fugger , 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, July 9–12, 2006, Sacramento, CA, AIAA-2006-4534 .
   Google Scholar
• B. J. McBride and S. Gordon , Computer Program for Calculation of Complex Chemical Equilibrium Compositions and Applications , vol. 1311 , NASA Reference Publication, American Institute of Aeronautics and Astronautics , Washington , DC , 2004 .
   Google Scholar
• P. J. Roache , Verification of Codes and Calculations , AIAA J. , vol. 36 , pp. 696 – 702 , 1998 .
   Google Scholar
• H. Schlichting and J. Kestin , Boundary-Layer Theory , vol. 539 , McGraw-Hill , New York , 1968 .
   Google Scholar