系統識別號 U0026-0802201710172300 論文名稱(中文) 複材飛機之最佳窗戶設計 論文名稱(英文) Optimization of Windows on Composite Aircraft 校院名稱 成功大學 系所名稱(中) 航空太空工程學系 系所名稱(英) Department of Aeronautics & Astronautics 學年度 105 學期 1 出版年 106 研究生(中文) 廖家聖 研究生(英文) Louis Bargé 學號 P46057030 學位類別 碩士 語文別 英文 論文頁數 88頁 口試委員 指導教授-胡潛濱口試委員-夏育群口試委員-楊文彬 中文關鍵字 none 英文關鍵字 Optimization  Composite fuselage  Aircraft  Window  ANSYS 學科別分類 中文摘要 none 英文摘要 In order to save computational time during optimization process, we want to know if optimization of simplified model can give us a trend to follow to improve much more complicated model. By running optimization process from the most general case, an infinite plate containing a hole under a traction loading to more complicated case, finite plate containing a hole with traction and pressure loading, we obtained results for a simplified model. Then we used these results into a more complicated problem. By using this approach, we optimize an aircraft composite fuselage panel. For these optimizations, we focused on mechanical part of this system, objective is to reduce the stress concentration factor. Results obtained with optimization procedure and results from the real model have similar trends. Therefor this procedure can be used to save a lot of optimization computational time. 論文目次 ABSTRACT I ACKNOWLEDGEMENTS II TABLE OF CONTENTS III LIST OF TABLES V LIST OF FIGURES VII CHAPTER I INTRODUCTION 1 1.1 Problem faced during complex model optimization 1 1.2. Literature review 2 CHAPTER II METHODOLOGY 3 2.1. Methodology presentation 3 2.2. Optimization problem 6 CHAPTER III PROCEDURE 22 3.1. Tools testing 22 3.1.1. Verifying ANSYS and AEPH results 22 3.1.2. Optimization’s trend check 23 3.2. Optimization process 33 3.2.1. Optimization of a finite plate containing a hole without pressure force. 33 3.2.2. Optimization of a finite plate containing a hole with pressure force. 34 3.3. Real model 36 3.3.1. Real model description 36 3.3.2. ANSYS modelling 40 CHAPTER IV RESULTS 48 4.1. Preliminary test 48 4.1.1. Test results 48 4.1.2. Optimization trend 50 4.2. Finite plate optimization 60 4.2.1. Finite plate without pressure force 60 4.2.2. Finite plate with pressure force 68 4.3. Real model 75 CHAPTER V CONCLUSION AND SUGGESTIONS 82 5.1. Conclusion 82 5.2. Suggestion 83 REFERENCES 85 參考文獻 [1] Ilhan, S., 2010, “Aircraft design fuselage study”. Master’s thesis, Delft University of Technology, Delft, Netherland. [2] Rouse, M. and Ambur, D. R., 1998, “Response of composite fuselage sandwich side panels subjected to internal pressure and axial tension”, AIAA/ASME/ASCE/AHS/ASC 35th Structural Dynamics, and Materials Conference, AIAA Paper No. 98-1708. [3] Mukhopadhyay, V. and Sobieszczanski-Sobieski, J., 2004, “Analysis, design, and optimization of noncylindrical fuselage for blended-wing-body Vehicle”, Journal of Aircraft, Vol. 41, No. 4, pp 925-930. [4] Sobieszczanski-Sobieski, J. and Loendorf, D., 1972, “A mixed optimization Method for Automated Design of Fuselage Structures”, Journal of Aircraft, Vol.9, No. 12, pp. 805-811. [5] Ungwattanapanit, T., and Baier, H., 2014, “Postbuckilng analysis and optimization of stiffened fuselage panels utilizing variable stiffness laminates”, International Council of Aeronautical Sciences 2014, Vol. 6, pp. 2321-2331 [6] Walker, T.h., Minguet, P. J., Carbery, D. J., Swanson, G. D. and Ilcewics, L. B, April 1997, “Advanced technology composite fuselage – Structural Performance”, NASA Contractor Report 4732. [7] Davis, G. W. and Sakata, I. F., March 1981, “Design consideration for composite fuselage structure of commercial transport Aircraft”, NASA Contractor Report 159296. [8] Rais-Rohani, M., “Design optimization and residual strength Assessment of a cylindrical composite shell structure”, 8th Symposium on Multidisciplinary analysis and Optimization, paper AIAA-2000-4742. [9] Hwu, C. and Yen, W. J., 1991, “Green’s functions of two-dimensional anisotropic plates containing an elliptic hole,” Int. J. Solids and Structures, Vol. 27, pp.1705-1719. [10] Arora, J. S., 2004. Introduction to optimum design, Elsevier Inc., Amsterdam. [11] ANSYS 16.0 Documentation: ANSYS Theory Reference for the Mechanical APDL and Mechanical Application. [12] Lekhnitskii, S. G., 1968. Anisotropic plates. Gordon and Breach, New York. [13] Singiresu, S. R., 2009. Engenieering Optimization, Theory and Practice, Fourth Edition. John Wiley & Sons, Inc., Hoboken, New Jersey. 論文全文使用權限 同意授權校內瀏覽/列印電子全文服務，於2017-02-13起公開。同意授權校外瀏覽/列印電子全文服務，於2017-02-13起公開。

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