【1】https://en.wikipedia.org/wiki/Ballistic_missile
【2】http://www.mdc.idv.tw/mdc/navy/usanavy/E-antiair-Missle-
Luancher.htm
【3】https://commons.wikimedia.org/w/index.php?curid=2001779
【4】Sutton G.P., Biblarz O. (2001), Rocket Propulsion Elements (7th
Edition), New York:John Wiley & Sons, Inc.
【5】徐文奇, “垂直發射裝置中燃氣兩相衝擊流場數值研究”, 哈爾
濱工程大學航天工程系碩士論文, 2007.
【6】Lee K. S, Hong S. K., “Supersonic Jet Impingement Navier-Stokes Computations for Vertical Launching System Design Applications”, Journal of Spacecraft and Rockets, Vol.41, No.5, October 2004.
【7】Nobuyuki T., A. Koichi H., Toshi F., Kazuo A., Masaru K., “Numerical Simulation of a Supersonic Jet Impingement on a Ground”, Journal of Aerospace, Vol. 100, Section 1, pp. 2168-2180, 1991.
【8】Gojon R., Bogey C., Marsden O., “Large-Eddy Simulation of Supersonic Planar Jets Impinging on a Flat Plate at an Angle of 60 to 90 Degrees”, 21st AIAA/CEAS Aeroacoustics Conference, June 2015.
【9】陳韋丞, “超音速高溫氣體衝擊擋板之數值模擬分析”, 成功大
學航空太空工程學系碩士論文,2019.
【10】Menter F. R., “Two Equation Eddy Viscosity Turbulence Models for Engineering Applications”, AIAA Journal, Vol. 32, No. 8, pp.1598-1605, 1994.
【11】宋緯倫, “不同紊流模式對超音速流場數值模擬結果之影響”,
成功大學航空太空工程學系碩士論文, 2010.
【12】郭忠義, “超音速高溫兩相流衝擊流場之模擬分析”, 成功大學航空太空工程學系碩士論文, 2020【13】York B. J., Sinha N., Dash S. M., Anderson L., Gominho L., Koo J.H., Cheung F. B., “Steady/Transient Plume-Launcher Interactions and Progress Towards Particulate/Surface Layer Modeling”, 33rd Aerospace Sciences Meeting and Exhibit, January 1995.
【14】Troyes J., Dubois I., Borie V., Boischot A., “Multi-phase Reactive Numerical Simulations of a Model Solid Rocket Motor Exhaust Jet”, 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, July 2006.
【15】Ma Y.J., Bao F.T., Xu H., Sun L., “Numerical Simulation of Solid Propellant Rocket Exhaust Plume Considering Two-Phase Flow Effects”, Applied Mechanics and Materials, Vol. 798, pp 185-189, October 2015.
【16】Feng S., Nie W., Xie Q., Duan L., “Numerical Simulation of Flow Field and Radiation of an Aluminized Solid-Propellant Rocket Multiphase Exhaust Plume”, 39th AIAA Thermophysics Conference, June 2007.
【17】Li Z., Wang N., Shi B., Li S., Yang R., “Effects of Particle Size on Two-Phase Flow Loss in Aluminized Solid Rocket Motors”, Acta Astronautic 159, pp.33-40,2019.
【18】Parker R. R., Klausner J.F., Mei R., “Supersonic Two-Phase Impinging Jet Heat Transfer”, Journal of Heat Transfer, Vol.135, Issue 2, pp.647-655, December 2012.
【19】林章裕, 林文山, 謝啟訓, “固態燃料推進器尾焰對於銅板之沖蝕試驗及熱傳模擬”, 中華民國第27屆燃燒與能源學術研討會, 論文編號016, April 2017.
【20】https://www.fangzhenxiuxiu.com/post/691478
【21】楊成麥, “噴霧模式之參數對液態燃料注入超音速流場數值模
擬分析影響之研究”, 成功大學航空太空工程學系碩士論文, 2019.
【22】http://www.wsbookshow.com/uploads/bookfile/201201/9787508492308_1.pdf
【23】ANSYS FLUENT 19.0 theory guide, ANSYS Inc.,2019
【24】Burak S., Caner Ekin Kiper, Bülent S., “Experimental and Numerical Investigation of Aluminum Particle Combustion in Solid Rocket Combustion Chambers”, 8th EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS),2019