匿蹤戰機是目前世界最先進的飛機製造技術，研發與製造匿蹤戰涉及許多技術，尤其是高推力引擎，當前全世界只有5個國家有能力研發高推力發動機，包括美、英、法、俄及中國，因此只有這些國家可以完做匿蹤戰機的設計及製造，另外一方面研發匿蹤戰機需要大量的資金，國家的經濟則是主要的軍費來源，本研究從二大面向來探台灣自行研發匿蹤戰機的可行性，研究結果顯示，台灣目前在經濟上要發展匿蹤戰機可能會排擠政府的其他支出，因為台灣的軍事費用支出已占政府支出的10%以上，比美國、日本的軍費比例都還要高出許多，加上經濟成長不高對發展匿蹤戰機也是一項不利的因素。另一方面對於匿蹤技術而言，台灣只有在結構性匿蹤複合材料可以達到100%的自製，其於的航電系統及高推力發動機技術正處於開始階段，因此認為台灣若要發展匿蹤戰機，在這方面參考日本、韓國及印度的做法，才將能研究的時間縮短，並增加成功的機率。

A stealth fighter is the most advanced aircraft in the world, and the development of the stealth fighter involves in many technologies, especially a high-thrust engine. So far there are only five countries, the United States of America, the Great Britain, the France, the Russia, and the China, capable of making high-thrust engines. Hence, they are eligible to fully develop their own stealth fighters. On the other hand, to develop a stealth fighter costs a lot, and most of the expenses is supported by the national budget. In this thesis, we discuss the feasibility of developing a stealth fighter from two aspects for Taiwan. We conclude that the budget to develop a stealth fighter may crowd out other expense of Taiwan government, since the budget of defence of Taiwan is higher than 10% of total government budget. The ratio is much higher than that of US or Japanese government. Moreover, the economic condition for Taiwan is not good recently, and this will worsen the budget problem. On the other hand, among all technologies required for a stealth fighter, Taiwan only owns the technology to make structural radar absorbing composite materials. Taiwan is still working on the development of avionics and high-thrust engines. Hence, by learning from the experience of Japan, Korea, and India, we can shorten the development time and increase the successful rate.

目錄
中文摘要	I
表目錄	IV
圖目錄	V
第1章	前言	1
1.1研究動機	1
1.2研究背景	4
1.3研究流程	6
第2章	匿蹤戰機與相關科技簡介	7
2.1匿蹤戰機之早期匿蹤技術	7
2.2 匿蹤戰機之先進結構型匿踨技術	9
2.3匿蹤戰機之雷達匿蹤技術	10
2.4匿蹤戰機之高推力發動機匿蹤技術	12
2.5 雷達吸收波複合材料匿蹤技術分析	15
2.6航電系統匿蹤技術分析探討	17
2.7高推力發動機系統技術分析	17
第3章	匿蹤戰機研發歷程興國家經濟力關係	20
3.1戰機世代發展回顧	20
3.2 目前世界匿蹤戰機研發概況介紹	24
3.3經濟實力對匿蹤技術的影響	29
3.3.1 世界各洲的軍事支出	30
3.3.2匿蹤戰機研發國家之軍事支出比較	30
3.3.3匿蹤戰機研發國家之軍事支出占國民生產毛額百分比比較	31
3.3.4匿蹤戰機研發國家之軍事支出占政府支出百分比分析	33
3.3.5匿蹤戰機研發國家之人均軍費開支分析	35
3.3.6匿蹤戰機研發成本分析	35
第4章	我國匿蹤戰機研發可行性分析	40
4.1從經濟的角度分析台灣發展匿蹤戰機的可行性	40
4.2從匿蹤戰機技術評估台灣發展匿蹤戰機的可行性	41
第5章	結論	44
參考文獻	46


 
表目錄
表格1: 各型發動機推力評估統計表	19
表格2: 世界各國第五代戰機介紹	25
表格3:全球各域區軍事支出統計表1992-2014	32
表格4: 研發匿蹤戰機國家軍事支出計表1992-2015	33
表格5: 研發匿蹤戰機國家軍事支出占國民生產毛額百分比1992-2015	36
表格6: 研發匿蹤戰機國家軍事支出占政府支出百分比1992-2015	37
表格7: 研發匿蹤戰機國家人均軍費開支1992-2015	38
表格8: 研發各型匿蹤戰機預算1992-2015	39

 
圖目錄
圖 1:研究流程圖	6
圖 2: US F-80 (前) 和GERMANY’S ME (後) 262	21
圖3: MIG-15 AND F-86 SABRE	21
圖 4: F-4 PHANTOM AND F-104	21
圖5: MIG-29(左)、F-16(右)、及IDF(下)	22
圖6: F-18 AND SU-30	23
圖7: PAK FA (T-50) AND SUKHOI SU-47	23
圖 8:第6代戰機示意圖	23
圖9:全球各區域軍事支出趨勢圖	33
圖10: 研發匿蹤戰機國家軍事支出	33
圖11: 研發匿蹤戰機國家軍事支出占國民生產毛額百分比	35
圖12: 研發匿蹤戰機國家軍事支出占政府支出百分比	39
圖13: 研發匿蹤戰機國家人均軍費開支	39

1中文參考文獻:
[1]	遲雅各、楊令樂、陳偉忠、莊達平、王正煥,2014.結構型匿蹤複合材料. 新新季刊,第42卷第2期,71-78.
[2]	陳和杰,2014.從近代戰爭探討軍事載具匿蹤技術運用與發展.陸軍學術雙月刊,第50卷第534期,138-152.
[3]	蕭丞鈞、陳信宏、侯元昌,2014.雙站雷達對隱形目標之偵測研究.新新季刊, 第42卷第1期,175-185.
2 英文參考文獻:
[4]	Chin, C., Kim, H., Setoguchi, T. & Matsuo, S. (2010), A computational study of thrust vectoring control using dual throat nozzle, J. Therm. Sci., 19(6): 486-490.
[5]	Chin W. S. & Lee D. G. (2011). Development of the composite RAS (radar absorbing structure) for the X-band frequency range, Composite Structures, 77 (4): 457-465.
[6]	Curtis, P. T. (1996). Multifunctional polymer composites, Advanced Performance Materials, 3 (3): 279–293.
[7]	Daniel IKAZA, D., & RAUSCH C. (2000). Thrust Vectoring for Eurofighter-The First Steps. AIR & SPACE EUROPE, 2 (1) : 92-95.
[8]	Ferlauto M., & Marsilio R. (2016). A numerical method for the study of fluidic thrust-vectoring. Advances in Aircraft and Spacecraft Science, 3 (4): 367-378.
[9]	Flamm, J. D., Deere, K. A., Mason, M. L., Berrier, B. L., & Johnson, S. K. (2006). Design enhancements of the two-dimensional, dual throat vectoring nozzle concept”,3rd AIAA Flow Control Conference, Control Conference, San Francisco, CA, USA.
[10]	Gama, A. M., Rezende M. C., & Dantas C. C. (2011). Dependence of microwave absorption properties on ferrite volume fraction in MnZn ferrite/rubber radar absorbing materials, Journal of Magnetism and Magnetic Materials, 323 (22): 2782-2785.
[11]	Rao, A. G. & Mahulikar, S. P. (2002). Integrated review of stealth technology and its role in airpower, Stealth Technology & Airpower, 106 (1066): 629-642.
[12]	Puttaswamy, P. & Murthy, P. S. K. (2013). Promising Stealth Technology Protocols in Defence, International Journal of Engineering Science Invention, 2 (10):18-22.
[13]	LUO, Z. B., XIA, Z. X., & XIE Y. G., (2007). Jet Vectoring Control Using a Novel Synthetic Jet Actuator. Chinese Journal of Aeronautics, 20, 193-201.
[14]	Mingxu Yi, M., Wang, L., & Huang, J. (2015). Active cancellation analysis based on the radar detection probability. Aerospace Science and Technology, 46, 273-281.
[15]	Oh, J. H., Oh K. S., Kim C. G., & Hong C. S. (2004). Design of radar absorbing structures using glass/epoxy composite containing carbon black in X-band frequency ranges, Composites Part B: Engineering, 35 (1): 49-56.
[16]	Wang, Y., Li T., Zhao L., & Gu, Z. H. Y. (2011). Research Progress on Nanostructured Rader Absorbing Materials, Energy and Power Engineering, 3, 580-584.
[17]	Xiaodong, Z., Bin, T., & Ying, X. (2012). Interception Algorithm of S-cubed Signal Model in Stealth Rader Equipment. Chinese Journal of Aeronautics, 25, 416-422.
[18]	Sheng, X. & Yuanming, X. (2012). Assemble An Active Cancellation Stealth System. Microwaves & rf, 51(7): 16.
[19]	Rudnik R., Rossow, C. C., & Geyr, H. F. V. (2002). Numerical simulation of engine/airframe integration for high-bypass engines. Aerospace Science and Technology, 6, 31-42.
[20]	Ryan Goldstein ,2017. Stealth Characteristics of the F-22 Raptor. Illumin, Volume XVIII Issue
[21]	Sanbongi, B. (1999). The Aircraft Engine: An Historical Perspective of Engine Development through World War I. Journal of Aviation Aviation Aerospace Education & Research, 8, 7-17.
[22]	Shin C. S., Kim H. D., Setoguchi T., & Mstsuo S., (2010). A computational study of thrust vectoring control using dual throat nozzle. Journal of Thermal Science, 19 (6): 486-490.
[23]	Smith B. L., & Glezer A. (2002). Jet vectoring using synthetic jets. J Fluid, 458, 1-34.
[24]	Tirpak, J. A. (2009, October). The Sixth Generation Fighter. Air Force Magazine, 38-42.
3.參考書目:
[25]	Hebert, A. J. (2008). Fighter Generations. AIR FORCE Magazine, 32-32.
[26]	Ufimtsev, P. Y. (1962). Method of Edge Waves in the Physical Theory of Diffraction. Soviet Radio.
4.參考網站:
[27]	維基百科 https://zh.wikipedia.org.
[28]	台灣維基百科 http://www.twwiki.com.
[29]	中時電子報 http://www.chinatimes.com/newspapers/20170427000168-260204.
[30]	經濟部航空產業推動小組 http://www.casid.org.tw/NewsView01.aspx?NewsID=862c6b6f-5abc-4842-8661-f617c4a93fb2.
[31]	聯合新聞網 https://udn.com/news/story/10776/2248707.