| 研究生: |
劉智恩 Liu, Chih-En |
|---|---|
| 論文名稱: |
應用代理模型優化155公厘榴彈於超音速下之幾何 Optimizing the Geometry of the 155mm Projectile for Supersonic Performance Using Surrogate-based Models |
| 指導教授: |
吳志勇
Wu, Chih-Yung |
| 學位類別: |
碩士 Master |
| 系所名稱: |
工學院 - 航空太空工程學系 Department of Aeronautics & Astronautics |
| 論文出版年: | 2024 |
| 畢業學年度: | 112 |
| 語文別: | 中文 |
| 論文頁數: | 133 |
| 中文關鍵詞: | 155公厘榴彈 、代理模型 、計算流體力學 、底排彈 、全域優化 |
| 外文關鍵詞: | 155mm projectile, Surrogate-based Model, Computational Fluid Dynamics(CFD), Base-bleed Projectile, Gobal optimization |
| 相關次數: | 點閱:69 下載:0 |
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[1] J. Ma, Z. Chen, D. Xue, and X. Sun, "Influences of boattail structures on aerodynamic characteristics of supersonic spinning projectiles," Theor Comp Fluid Dyn, vol. 34, pp. 249-270, 2020.
[2] M. A. Dali, S. Jaramaz, D. Jerković, and D. Djurdjevac, "Increasing the Range of Contemporary Artillery Projectiles," Tehnički vjesnik, vol. 26, no. 4, pp. 960-969, 2019.
[3] X. Xue and Y. Yu, "An improvement of the base bleed unit on base drag reduction and heat energy addition as well as mass addition," Applied Thermal Engineering, vol. 109, pp. 238-250, 2016.
[4] M. A. Dali and S. Jaramaz, "Optimization of artillery projectiles base drag reduction using hot base flow," Thermal Science, vol. 23, no. 1, pp. 353-364, 2019.
[5] 蔡旻橋, "超音速榴彈砲氣動力分析," 碩士, 航空太空工程學系碩士在職專班, 國立成功大學, 台南市, 2023. [Online]. Available: https://hdl.handle.net/11296/8bcujm
[6] 王景平, "155公厘底凹型榴彈氣動力特性分析," 碩士, 機械工程碩士班, 國防大學理工學院, 桃園縣, 2020. [Online]. Available: https://hdl.handle.net/11296/x7n8tj
[7] R. L. McCoy, MC DRAG-a computer program for estimating the drag coefficients of projectiles. US Army Armament Research and Development Command, Ballistic Research Laboratory, 1981.
[8] R. L. McCoy, Modern exterior ballistics: The launch and flight dynamics of symmetric projectiles. Schiffer Pub., 1999.
[9] L. D. Kayser and F. Whiton, Surface pressure measurements on a boattailed projectile shape at transonic speeds. Ballistic Research Laboratory, 1982.
[10] M. Miller, "Wind tunnel measurements of the Magnus induced surface pressures on a spinning projectile in the transonic speed regime," in Applied Aerodynamics Conference, 1983, p. 1838.
[11] J.-K. FU and S.-M. LIANG, "A numerical study on drag reduction for turbulent transonic flow over a projectile," in 27th Joint Propulsion Conference, 1991, p. 2260.
[12] M. Suliman, O. Mahmoud, M. Al-Sanabawy, and O. Abdel-Hamid, "Computational investigation of base drag reduction for a projectile at different flight regimes," in International Conference on Aerospace Sciences and Aviation Technology, 2009, vol. 13, no. AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT-13, May 26–28, 2009: The Military Technical College, pp. 1-13.
[13] J. Sahu, "Supersonic flow over cylindrical afterbodies with base bleed," Computational mechanics, vol. 2, no. 3, pp. 176-184, 1987.
[14] J.-K. Fu and S.-M. Liang, "Drag reduction for turbulent flow over a projectile: Part I," J Spacecraft Rockets, vol. 31, no. 1, pp. 85-92, 1994.
[15] H. Bournot, E. Daniel, and R. Cayzac, "Improvements of the base bleed effect using reactive particles," Int J Therm Sci, vol. 45, no. 11, pp. 1052-1065, 2006.
[16] P. Kaurinkoski and A. Hellsten, "Numerical simulation of a supersonic base-bleed projectile with improved turbulence modeling," J Spacecraft Rockets, vol. 35, no. 5, pp. 606-611, 1998.
[17] F. Simon, S. Deck, P. Guillen, and R. Cayzac, "Numerical simulations of projectile base flow," in 44th AIAA Aerospace Sciences Meeting and Exhibit, 2006, p. 1116.
[18] A. Ferfouri, T. Allouche, D. D. Jerković, N. Hristov, M. Vučković, and A. Benmeddah, "PREDICTION OF DRAG AERODYNAMIC COEFFICIENT OF THE 155MM PROJECTILE UNDER AXISYMMETRIC FLOW USING DIFFERENT APPROACHES," Journal of the Serbian Society for Computational Mechanics/Vol, vol. 17, no. 2, pp. 69-86, 2023.
[19] S. Jeong, S. Obayashi, and K. Yamamoto, "Aerodynamic optimization design with Kriging model," Transactions of the Japan society for Aeronautical and Space Sciences, vol. 48, no. 161, pp. 161-168, 2005.
[20] G. Arnoult, M. Zeidler, and E. Garnier, "Optimization Methodology for a 2-D Course Correction of a 155 mm Spin-Stabilized Projectile," in 2018 Applied Aerodynamics Conference, 2018, p. 3950.
[21] G. Arnoult, M. Zeidler, and E. Garnier, "Control surface geometry surrogate-based optimization for spin-stabilized projectile course correction," AIAA journal, vol. 58, no. 2, pp. 550-560, 2020.
[22] B. Xing, C. Du, Z. Du, and W. Yang, "Robust Optimization Design of the Aerodynamic Shape and External Ballistics of a Pulse Trajectory Correction Projectile," Applied Sciences, vol. 13, no. 12, p. 7007, 2023.
[23] G. Nikishkov, "Introduction to the finite element method," University of Aizu, pp. 1-70, 2004.
[24] F. Moukalled, L. Mangani, M. Darwish, F. Moukalled, L. Mangani, and M. Darwish, The finite volume method. Springer, 2016.
[25] A. Fluent, "Ansys fluent theory guide," Ansys Inc., USA, vol. 15317, pp. 724-746, 2011.
[26] A. N. Kolmogorov, "Dissipation of energy in isotropic turbulence," in Dokl. Akad. Nauk SSSR, 1941, vol. 32, pp. 325-327.
[27] A. N. Kolmogorov, "The local structure of turbulence in incompressible viscous fluid for very large Reynolds numbers," Proceedings of the Royal Society of London. Series A: Mathematical and Physical Sciences, vol. 434, no. 1890, pp. 9-13, 1941.
[28] F. G. Schmitt, "About Boussinesq’s turbulent viscosity hypothesis: historical remarks and a direct evaluation of its validity," Comptes Rendus Mécanique, vol. 335, no. 9-10, pp. 617-627, 2007.
[29] P. Spalart and S. Allmaras, "A one-equation turbulence model for aerodynamic flows," in 30th aerospace sciences meeting and exhibit, 1992, p. 439.
[30] B. E. Launder and D. B. Spalding, "The numerical computation of turbulent flows," in Numerical prediction of flow, heat transfer, turbulence and combustion: Elsevier, 1983, pp. 96-116.
[31] V. Yakhot, S. A. Orszag, S. Thangam, T. Gatski, and C. Speziale, "Development of turbulence models for shear flows by a double expansion technique," Physics of Fluids A: Fluid Dynamics, vol. 4, no. 7, pp. 1510-1520, 1992.
[32] T.-H. Shih, W. W. Liou, A. Shabbir, Z. Yang, and J. Zhu, "A new k-ϵ eddy viscosity model for high reynolds number turbulent flows," Computers & fluids, vol. 24, no. 3, pp. 227-238, 1995.
[33] D. C. Wilcox, "Reassessment of the scale-determining equation for advanced turbulence models," AIAA journal, vol. 26, no. 11, pp. 1299-1310, 1988.
[34] F. R. Menter, "Improved two-equation k-omega turbulence models for aerodynamic flows," 1992.
[35] F. R. Menter, "Two-equation eddy-viscosity turbulence models for engineering applications," AIAA journal, vol. 32, no. 8, pp. 1598-1605, 1994.
[36] F. R. Menter, M. Kuntz, and R. Langtry, "Ten years of industrial experience with the SST turbulence model," Turbulence, heat and mass transfer, vol. 4, no. 1, pp. 625-632, 2003.
[37] A. Wimshurst. Fluid Mechanics 101 [Online] Available: https://www.fluidmechanics101.com/pages/lectures.html
[38] D. M. Mckay, Beckman, R., and Conover, W., "A Comparison of Three Methods for Selecting Values of Input Variables in the Analysis of Output From a Computer Code," Technometrics, vol. 21, pp. 239-245, 1979.
[39] M. D. Morris and T. J. Mitchell, "Exploratory designs for computational experiments," Journal of statistical planning and inference, vol. 43, no. 3, pp. 381-402, 1995.
[40] A. Forrester, A. Sobester, and A. Keane, Engineering design via surrogate modelling: a practical guide. John Wiley & Sons, 2008.
[41] A. I. Forrester, A. Sóbester, and A. J. Keane, "Multi-fidelity optimization via surrogate modelling," Proceedings of the royal society a: mathematical, physical and engineering sciences, vol. 463, no. 2088, pp. 3251-3269, 2007.
[42] A. J. K. Alexander I.J. Forrester, "Recent advances in surrogate-based optimization," Progress in Aerospace Sciences, vol. 45, no. 1-3, pp. 50-79, 2009, doi: https://doi.org/10.1016/j.paerosci.2008.11.001.
[43] S. Koziel and L. Leifsson, Simulation-driven design by knowledge-based response correction techniques. Springer, 2016.
[44] C. K. Williams and C. E. Rasmussen, Gaussian processes for machine learning (no. 3). MIT press Cambridge, MA, 2006.
[45] X. Yang, D. Barajas-Solano, G. Tartakovsky, and A. M. Tartakovsky, "Physics-informed CoKriging: A Gaussian-process-regression-based multifidelity method for data-model convergence," Journal of Computational Physics, vol. 395, pp. 410-431, 2019.
[46] M. Wessam and Z. Chen, "Firing precision evaluation for unguided artillery projectile," in 2015 International Conference on Artificial Intelligence and Industrial Engineering, 2015: Atlantis Press, pp. 584-587.
[47] "Examining Spatial (Grid) Convergence." NPARC Alliance CFD Verification and Validation Web site. https://www.grc.nasa.gov/www/wind/valid/tutorial/spatconv.html (accessed.
[48] P. J. Roache, Verification and validation in computational science and engineering. Hermosa Albuquerque, NM, 1998.
[49] E. M. Youssef, M. A. Radwan, H. E. Mostafa, and M. K. Hadhoud, "Low signature advanced base bleed grains," International Journal of Scientific & Engineering Research, vol. 6, no. 12, pp. 980-985, 2015.
[50] M.-S. Liou, "A sequel to AUSM, Part II: AUSM+-up for all speeds," Journal of computational physics, vol. 214, no. 1, pp. 137-170, 2006.
[51] M. J. Andrew Heather , Mark Olesen,Kutalmış Berçin,Matej Forman,Matej Forman,Pawan Ghildiyal,Chiara Pesci,Fred Mendonça,Swapnil Salokhe,Jiri Polansky,OpenCFD Ltd,Jozsef Nagy, "Open∇FOAM:The Open Source CFD Toolbox, User and Theory Guide v2312," 2023. [Online]. Available: https://doc.openfoam.com/2312/
[52] J. P. S. Vale, "Aerothermodynamic analysis of an experimental rocket aimed to test micro-launcher technologies," Universidade da Beira Interior (Portugal), 2022.
[53] "High Speed Aerodynamic Solver:User Guide," CSIR, 2021.
[54] J. A. Heyns, O. F. Oxtoby, and A. Steenkamp, "Modelling high-speed flow using a matrix-free coupled solver," in Proceedings of the 9th OpenFOAM Workshop, Zagreb, Croatia, 2014, pp. 23-26.
[55] P. Das and A. De, "Numerical study of flow physics in supersonic base-flow with mass bleed," Aerospace Science and Technology, vol. 58, pp. 1-17, 2016.
[56] X. Yang, Y. Hu, Z. Gong, J. Jian, and Z. Liu, "Numerical study of combined drag reduction bases on vortex generators and riblets for the ahmed body using IDDES methodology," Journal of Applied Fluid Mechanics, vol. 15, no. 1, pp. 193-207, 2021.
校內:2029-08-13公開