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발사체 해석을 위한 CFD 소프트웨어 적용 현황

Present State of CFD Softwares Application for Launch Vehicle Analysis

  • 투고 : 2020.01.14
  • 심사 : 2020.04.17
  • 발행 : 2020.06.30

초록

발사체 분석을 위한 CFD 소프트웨어인 LVAFoam을 개발하기 앞서 발사체의 연소기, 터보 펌프 및 외부유동의 시뮬레이션에 사용된 해외의 인하우스 CFD 소프트웨어 및 상용 CFD 소프트웨어에 대한 조사를 수행하였다. 인하우스 소프트웨어로는 NASA, 미시시피 주립대학, DLR, Bertin Technologies & CNES, CERFACS 및 JAXA의 솔버들과, 상용 소프트웨어로는 FLUENT, CFX, Adavance/FrontFlow/red, GASP, CRUNCH CFD, CFD-ACE+, FINETM/Turbo, STAR-CCM+ 의 솔버들을 정리하였다. 발사체 분석을 위한 각 소프트웨어의 계산 사례가 제시되었으며, 개발된 LVAFoam이 간략하게 소개되었다.

Before we develop LVAFoam, a CFD software for launch vehicle analysis, we conducted a survey on other CFD softwares. We looked at in-house code and commercial CFD software of other countries that were used as a simulation of launch vehicle's combustor, turbopump and external flow. This research included in-house code solvers, developed by NASA, Mississippi State University, DLR, Bertin Technologies, CNES, CERFACS, and JAXA as well as commercial CFD software from FLUENT, CFX, Advance/FrontFlow/red, GASP, CRUNCH CFD, CFD-ACE+, FINETM/Turbo, STAR-CCM+. The simulation cases of launch vehicle analysis from each commercial softwares and introduction of the LVAFoam were presented.

키워드

과제정보

본 논문은 정부(과학기술정보통신부)의 재원으로 한국연구재단 우주핵심기술개발사업(2017M 1A3A3A03015993, 2017M 1A3A3A 04016580)의 지원으로 작성되었습니다.

참고문헌

  1. CFD Online, World Wide Web location http://www.cfd-online.com/Wiki/Codes.
  2. NASA Software Catalog 2017-2018, World Wide Web location http://software.nasa. gov/NASA_Software_Catalog_2017-18.pdf, 2018.
  3. Dissel, A.F., Huseman, P.G., Bomba, J.V., Mayfield, D.P., Voorhees, S.B. and Hellman, B.M., "Aft End Heating Assessment of Multiple Engine Clusters for a Reusable First Stage Launch Vehicle," AIAA Space 2012 Conference & Exposition, p. 5281, 2012.
  4. Gusman, M., Housman, J. and Kiris, C., "Best Practices for CFD Simulation of Launch Vehicle Ascent with Plumes-Overflow Perspective," 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, p. 1054, 2011.
  5. Dalle, D.J., "Launch Vehicle Aerodynamics Database Development for SLS," Advanced Modeling & Simulation Seminar, 2018.
  6. Kiris, C., Kwak, D. and Chan, W., "Parallel Unsteady Turbopump Simulations for Liquid Rocket Engines," Proceedings of the IEEE/ACM SC2000 Conference, 2000.
  7. Edquist, K.T., Korzun, A.M., Bibb, K.L., Schauerhamer, D.G., Ma, E.C., McCloud, P.L., Palmer, G.E. and Monk, J.D., "Comparison of Navier-Stokes Flow Slovers to Falcon 9 Supersonic Retropropulsion Flight Data," AIAA Space and Astronautics Forum and Exposition, p. 5296, 2017.
  8. Kiris, C.C., Housman, J.A., Barad, M.F., Sozer, F., Brehm. C. and Moini-Yekta. S., "Computational Framework for Launch, Ascent, and Vehicle Aerodynamics(LAVA)," Aerospace Science and Technology, Vol. 55, pp. 189-219, 2016. https://doi.org/10.1016/j.ast.2016.05.008
  9. Lin, J., West, J.S., Williams, R.W., Tucker, P.K. and Chenoweth, J.D., "CFD Code Validation of Wall Heat Fluxes for a GO2/GH2 Single Element Combustor," 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, p. 4524, 2005.
  10. Schwambom, D., Gardner, A.D., von Geyr, H., Krumbein, A., Ludeke, H. and Sturmer, A., "Development of the DLR TAU-Code for Aerospace Applications," International Conference on Aerospace Science and Technology, pp. 26-28, 2008.
  11. Lempke, M., Gerlinger, P., Aigner, M. and Rachner, M., "Steady and Unsteady RANS Simulation of Cryogenic Rocket Combustors," 49th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, p. 101, 2011.
  12. Roth, C., Haidn, O., Chemnitz, A., Sattelmayer, T., Daimon, Y., Frank, G., Muller, H., Zips, J., Pfitzner, M., Keller, R., Gerlinger, P., Maestro, D., Cuenot, B., Riedmann, H. and Selle, L., "Numerical Investigation of Flow and Combustion in a Single Element GCH4/Gox Rocket Combustor," 52nd AIAA/SAE/ASEE Joint Propulsion Conference, p. 4995, 2016.
  13. Zmijanovic, V., Leger, L., Depussay, E., Sellam, M. and Chpoun, A., "Experimental-Numerical Parametric Investigation of a Rocket Nozzle Secondary Injection Thrust Vectoring," Journal of Propulsion and Power, Vol. 32, pp. 196-213, 2016. https://doi.org/10.2514/1.B35721
  14. Legrand, B., Durand, P. and Vuillermoz, P., "Test Case RCM-3 using CPS," CNES ADP012370, 2001.
  15. Urbano, A., Selle, L., Staffelbach, G., Cuenot, B., Schmitt, T., Ducruix, S. and Candel, S., "Exploration of Combustion Instability Triggering using Large Eddy Simulation of a Multiple Injector Liquid Rocket Engine," Combustion and Flame, Vol. 169, pp. 129-140, 2016. https://doi.org/10.1016/j.combustflame.2016.03.020
  16. Kitamura, K., Nonaka, S., Kuzuu, K., Aono, J., Fujimoto, K. and Shima, E., "Numerical and Experimental Investigations of Epsilon Launch Vehicle Aerodynamics at Mach 1.5," Journal of Spacecraft and Rockets, Vol. 50 No. 4, pp. 896-916, 2013. https://doi.org/10.2514/1.A32284
  17. Tsutsumi, S., Takaki, R., Koike, S. and Teramoto, S., "Application of Hybrid Turbulence Method to Transonic Flowfield of a Payload Fairing," 54th AIAA Aerospace Sciences Meeting, p. 0554, 2016.
  18. RESOLVED analytics, Comparing CFD Software, https://www.resolvedanalytics.com/theflux/comparing-cfd-software, 2018.
  19. Daimon, Y., Ohnishi, Y., Negishi, H. and Yamanishi, N., "Combustion and Heat Transfer Modeling in Regeneratively Cooled Thrust Chambers (Co-axial Injector Flow Analysis)," 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, p. 5492, 2009.
  20. Singhal, A., Tharakan, T.J. and Thomas, R.P., "CFD Analysis of Water Cooled Flame Deflector in Rocket Engine Test Facility," Fluid Mechanics and Fluid Power-Contemporary Research, pp. 517-528, 2017.
  21. Murray, W.L., Steiner, M.W., Neal, J.A. and Hunt, S.A., "Design and Analysis of a High Speed, High Pressure Peroxide/RP-1 Turbopump," 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, p. 3499, 2014.
  22. Engblom, W.A., "Numerical Simulation of Titan IVB Transonic Buffet Environment," Journal of Spacecraft and Rockets, Vol. 40, No. 5, pp. 648-656, 2003. https://doi.org/10.2514/2.6913
  23. Daimon, Y., Negishi, H. and Kawashima, H., "Film Cooling Performance Analysis of a Full-Scale Liquid Rocket Engine Combustion Chamber Based on a Coupled Combustion and Heat Transfer Simulation," 53rd AIAA/SAE/ASEE Joint Propulsion Conference, p. 4919, 2017.
  24. Negishi, H., Ohno, S., Ogawa, Y., Aoki, K., Kobayashi, T., Okita, K. and Mizuno, T., "Numerical Analysis of Unshrouded Impeller Flowfield in the LE-X Liquid Hydrogen Pump," 53rd AIAA/SAE/ASEE Joint Propulsion Conference, p. 4930, 2017.
  25. Allgood, D. and Ahuja, V., "Computational Plume Modeling of Conceptual ARES Vehicle Stage Tests," 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, p. 5708, 2007.
  26. Sachdev, J.S., Ahuja, V., Hosangadi, A. and Allgood, D.C., "Analysis of Flame Deflector Spray Nozzles in Rocket Engine Test Stands," 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, p. 6972, 2010.
  27. Kirchberger, C., Hupfer, A., Kau, H.P., Soller, S., Martin, P., Bouchez, M. and Dufour, E., "Improved Prediction of Heat Transfer in a Rocket Combustor for GOX/Kerosene," 47th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, p. 1214, 2009.
  28. Coutier-Delgosha, O., Fortes-Patella, R., Reboud, J.L., Hakimi, N. and Hirsch, C., "Numerical Simulation of Cavitating Flow in 2D and 3D Inducer Geometries," International Journal for Numerical Methods in Fluids, Vol. 48, No. 2, pp. 135-167, 2005. https://doi.org/10.1002/fld.820
  29. Pouffary, B., Patella, R.F., Reboud, J.L. and Lambert, P.A., "Numerical Simulation of 3D Cavitating Flows: Analysis of Cavitation Head Drop in Turbomachinery," Journal of Fluids Engineering, Vol. 130, No. 6, 061301, 2008. https://doi.org/10.1115/1.2917420
  30. GONZALEZ, M.V.J., "Numerical Computation of Transonic Loads on Ariane 5ECA during Launch Phase," Master's Degree, Universita di Pisa, Italia, 2013.
  31. Kim, T.W. and Shin, J.R., "Enhanced Pressure Based Coupled Algorithm to Combine with Pressure-Velocity-Enthalpy for All Mach Number Flow," Journal of Computational Fluids Engineering, Vol. 23, No. 4, pp. 64-73, 2018. https://doi.org/10.6112/kscfe.2018.23.4.064