Luận án Buckling analysis of inflatable composite beams
This thesis presents a numerical modeling and an experimental program
approach to investigate the buckling behavior of inflatable beams made from woven
fabric composite materials.
In the numerical study, the Isogeometric Analysis (IGA) is utilized to analyze
the bucking response of inflatable beams subject to axial compressive load and
predict the critical load at which the first wrinkle occurs. In the numerical model, the
Timoshenko’s kinematics principle is used to build a 3D model of inflating
orthotropic beams. In this modeling process, geometrical non-linearity is
considerated by using the energy concept that accounts for the change in membrane
and strain energies when the beams are bent. By using Lagrangian and virtual work
principles, nonlinear equilibrium equations were derived. These equations are then
discretized by using NURBS basis functions inherited from IGA approach to derive
the global nonlinear equation. The well-known Newton-Raphson algorithm is then
used to solve the nonlinear equation. The numerical results are then calibrated with
the experimental one. It was found that a good agreement between IGA predictions
and test results is achieved. The numerical model could be used for other parametric
studies to investigate the influences of material and geometrial parameters on the
buckling behaviour of inflatable beams.
In the experiment study, the mechanical properties of the woven fabric
composite material used in frabrication of inflatable beams are determined and the
biaxial buckling test is carried out. The experimental studies are performed under
various inflation pressures to characterize the orthotropic mechanical properties and
the nonlinear buckling behaviors. Load versus deflection curve of inflating beams
beam with different air pressures obtained from the experimentsare are illustrated.,
and the first wrinkles of the beams when buckling happens is also monitored.
Therefore, the maximum load carrying capacity of the inflating beam with respect to
the appearance of the first wrinkle is totally found. In addition, the critical bucklingvii
load is determined through distinct load cases. Then, the discrepancy is evaluated
among the proposed orthotropic and isotropic models in literature.
Tóm tắt nội dung tài liệu: Luận án Buckling analysis of inflatable composite beams
MINISTRY OF EDUCATION AND TRAINING HCM CITY UNIVERSITY OF TECHNOLOGY AND EDUCATION ---oo0oo--- PHAN THI DANG THU BUCKLING ANALYSIS OF INFLATABLE COMPOSITE BEAMS PHD THESIS MAJOR: MECHANICAL ENGINEERING CODE: 9520103 HCM City, August 2021 MINISTRY OF EDUCATION AND TRAINING HCM CITY UNIVERSITY OF TECHNOLOGY AND EDUCATION --- oOo --- PHAN THI DANG THU BUCKLING ANALYSIS OF INFLATABLE COMPOSITE BEAMS MAJOR: MECHANICAL ENGINEERING CODE: 9520103 Supervisor one : Assoc. Prof. Dr. Phan Dinh Huan Supervisor two : Assoc. Prof. Dr. Le Hieu Giang Reviewer 1: Reviewer 2: Reviewer 3: HCM City, August 2021 i LÝ LỊCH CÁ NHÂN I. LÝ LỊCH SƠ LƯỢC Họ và tên: PHAN THỊ ĐĂNG THƯ Giới tính: Nữ Ngày, tháng, năm sinh: 05/11/1977 Nơi sinh: Tiền Giang Quên quán: Tiền Giang Dân tộc: Kinh Học vị cao nhất: Thạc Sỹ Kỹ thuật Đơn vị công tác: Trường Cao Đẳng Công Nghệ Thủ Đức Chỗ ở riêng hoặc địa chỉ liên lạc: B2-14/09 c/c Lê Thành, Phường An Lạc, Quận Bình Tân, TP.HCM Điện thoại liên hệ: 0903373645 Email: dangthu0511@yahoo.com II. QUÁ TRÌNH ĐÀO TẠO 1. Đại học: - Hệ đào tạo: Chính qui - Nơi đào tạo: Trường Đại học Sư phạm Kỹ thuật TP. HCM - Ngành học: Kỹ thuật công nghiệp - Năm tốt nghiệp: 2000 2. Sau đại học - Hệ đào tạo: Chính qui - Nơi đào tạo: trường Đại học Sư phạm Kỹ thuật Tp. HCM - Việt Nam - Thạc sĩ chuyên ngành: Kỹ thuật cơ khí - Năm tốt nghiệp: 2004 III. QUÁ TRÌNH CÔNG TÁC - 2000-2005: Giảng viên - Trường Cao đẳng Bán công Công nghệ và quản trị doanh nghiệp. - 2005-2019: Giảng viên, Trưởng khoa Cơ khí - Trường Cao đẳng nghề TPHCM - 2019-2020: Giảng viên, Giám đốc trung tâm - Viện khoa học An toàn vệ sinh lao động TPHCM - 2020 đến nay: Giảng viên - Trường Cao đẳng Công nghệ Thủ Đức TPHCM IV. LĨNH VỰC CHUYÊN MÔN - CAD/CAM/CNC - Gia công CNC - Thiết kế kỹ thuật cơ khí V. CÁC CÔNG TRÌNH ĐÃ CÔNG BỐ Số TT NỘI DUNG 1 T. Le-Manh, Q. Huynh-Van, Thu D. Phan, Huan D. Phan, H. Nguyen-Xuan “Isogeometric nonlinear bending and buckling analysis of variablethickness composite plate structures”; Composite Structures 1 January 2017, Pages 818-826. 2 Phan Thi Dang Thu, Phan Dinh Huan and Nguyen Thanh Truong “Effect parametric to properties of a 2D orthogonal plain classical woven fabric composite”; ISBN: 978-604-913-367-1, pages 509-517. 3 Phan Thi Dang Thu, Phan Dinh Huan and Nguyen Thanh Truong “Biaxial beam inflation test on orthotropic fabric beam”; ISBN: 978-604-913-213-1, pages 1169-1176. 4 Nguyen Thanh Truong, Phan Dinh Huan, Phan Thi Dang Thu “Discretizing an analytical inflating beam model by the shellmembrane finite elelment”; ISBN: 978-604-913-213-1, pages 1221-1228. 5 Phan Thi Dang Thu, Le Manh Tuan, Nguyen Xuan Hung, Nguyen Thanh Truong “Geometrically nonlinear behaviour of composite beams of variable fiber volume fraction in isogeometric analysis”; ISBN: 978-604-82-2028-0, Pages: 1404-1409. 6 Thu Phan-Thi-Dang, Tuan Le-Manh, Giang Le-Hieu, Truong Nguyen- Thanh “Buckling of cylindrical inflating composite beams using isogeometric analysis”; ISBN: 978-604-73-3691-3, Pages 821-826. iii Số TT NỘI DUNG 7 Phan Thi Dang Thu, Nguyen Thanh Truong, Phan Dinh Huan “Mô hình dầm hơi composite phi tuyến chịu uốn”; ISBN: 976-604-82-2026-6, Page 697-704. 8 Phan Thi Dang Thu, Nguyen Thanh Truong, Phan Dinh Huan, Le Dinh Tuan “Biaxial experiments for determining material properties and joint strength of textile plain woven fabric composites”; ISBN: 978-604-913-722- 8, Page 1174-1181. TP. HCM, ngày 12 tháng 8 năm 2021 Nghiên cứu sinh Phan Thị Đăng Thư ORIGINALITY STATEMENT I, Phan Thị Đăng Thư, hereby assure that this dissertation is my own work, done under the guidance of Assoc. Prof. Dr. Phan Dinh Huan and Assoc. Prof. Dr. Le Hieu Giang with the best of my knowledge. All results and data that are stated and presented in this dissertation are honest. And they have not been published by any previous works. Ho Chi Minh City, August 2021 Phan Thi Dang Thu v ACKNOWLEDGEMENTS The dissertation is implemeted at the Faculty of Mechanical Engineering, Ho Chi Minh City University of Technology and Education, Viet Nam. The conducting process of this thesis not only brings motivation, but it also takes several challenges and difficulties. Without any support and coopperating by my professors, colleagues as well as my students, this thesis would not be achieved completely and fluently. That is why, first of all, I would like to express my appreciation to Assoc. Prof. Phan Dinh Huan and Assoc. Prof. Le Hieu Giang, for accepting me as a PhD student and for their enthusiastic guidance during my research. Moreover, I would like to kindly thank Dr. Nguyen Thanh Truong, Dr. Le Manh Tuan, Mr. Duong Chi Hung (a young brothers), for their helpful supporting in every first steps of doing research. They conscientiously helped me to overcome during my hardest time. Secondly, I would like to acknowledge Assoc. Prof. Le Dinh Tuan, Faculty of Transportation Engineering, Ho Chi Minh City University of Technology, Vietnam, who troubleshooted my troubles and helped to solve problems incidentally occurring in my study. Thirdly, I also take this chance to thank all my talent colleagues for their professional instruction and advice, as well as to my lovely students for their nicely support. Last but not least, the family’s love and encouragement are definitely my biggest motivation. They gave me plenty of valuable assistance with their love and affection. Phan Thi Dang Thu ABSTRACT This thesis presents a numerical modeling and an experimental program approach to investigate the buckling behavior of inflatable beams made from woven fabric composite materials. In the numerical study, the Isogeometric Analysis (IGA) is utilized to analyze the bucking response of inflatable beams subject to axial compressive load and predict the critical load at which the first wrinkle occurs. In the numerical model, the Timoshenko’s kinematics principle is used to build a 3D model of inflating orthotropic beams. In this modeling process, geometrical non-linearity is considerated by using the energy concept that accounts for the change in membrane and strain energies when the beams are bent. By using Lagrangian and virtual work principles, nonlinear equilibrium equations were derived. These equations are then discretized by using NURBS basis functions inherited from IGA approach to derive the global nonlinear equation. The well-known Newton-Raphson algorithm is then used to solve the nonlinear equation. The numerical results are then calibrated with the experimental one. It was found that a good agreement between IGA predictions and test results is achieved. The numerical model could be used for other parametric studies to investigate the influences of material and geometrial parameters on the buckling behaviour of inflatable beams. In the experiment study, the mechanical properties of the woven fabric composite material used in frabrication of inflatable beams are determined and the biaxial buckling test is carried out. The experimental studies are performed under various inflation pressures to characterize the orthotropic mechanical properties and the nonlinear buckling behaviors. Load versus deflection curve of inflating beams beam with different air pressures obtained from the experimentsare are illustrated., and the first wrinkles of the beams when buckling happens is also monitored. Therefore, the maximum load carrying capacity of the inflating beam with respect to the appearance of the first wrinkle is totally found. In addition, the critical buckling vii load is determined through distinct load cases. Then, the discrepancy is evaluated among the proposed orthotropic and isotropic models in literature. Contents BIOGRAPHY ............................................................................................................ I ORIGINALITY STATEMENT ............................................................................ IV ACKNOWLEDGEMENTS ..................................................................................... V ABSTRACT ............................................................................................................ VI CONTENTS ......................................................................................................... VIII NOTATIONS AND CONVENTIONS ................................................................ XII LIST OF FIGURE ............................................................................................ XVIII LIST OF TABLE .............................................................................................. XXIII CHAPTER 1: INTRODUCTION ............................................................................ 1 1.1 Background information ....................................................................................... 1 1.2 Motivation of the thesis ......................................................................................... 2 1.3 The objectives and scope of the study .................................................................. 2 1.4 Methodology ......................................................................................................... 3 1.5 Outline of the thesis .............................................................................................. 4 1.6 Original contributions of the thesis ....................................................................... 5 1.7 Significances of the thesis ..................................................................................... 5 CHAPTER 2: LITERATURE REVIEW ................................................................ 7 2.1 An overview of fibous composite materials ......................................................... 7 2.1.1 Fiber types ...................................................................................................... 9 2.1.2 Matrix Materials .......................................................................................... 13 2.1.3 Composite Properties ................................................................................... 14 2.1.4 Advantages of composite ............................................................................. 15 2.2 Practical applications of inflating composite structures ..................................... 18 2.2.1 Aerospace ..................................................................................................... 19 2.2.2 Civil engineering and architecture ............................................................... 21 2.2.3 Other fields of application ........................................................................... 22 ix 2.3 Anal ... 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[128] Zouani, A., Bui-Quoc, T., and Bernard, M. (1999). Cyclic stress-strain data analysis under biaxial tensile stress state. Exp Mech, 39:92–102. [129] Almroth, B.O., Holmes, A.M.C. & Brush, D.O. (1964). An experimental study of the bucking of cylinders under axial compression. Experimental Mechanics 4, 263–270. [130] Nguyen, T.T, Ronel, S., Massenzio, M., Jacquelin, E., Apedo, K.L., Phan-Dinh, H. (2013) Numerical buckling analysis of an inflatable beam made of orthotropic technical textiles, Thin-Walled Structures 72. 61-75. List of publications 164 List of Publications Parts of this dissertation have been published in international journals, national journals or presented in conferences. These papers are: • Articles in international scientific journal 1. T. Le-Manh, Q. Huynh-Van, Thu D. Phan, Huan D. Phan, H. Nguyen- Xuan “Isogeometric nonlinear bending and buckling analysis of variablethickness composite plate structures”. Composite Structures 2017, Pages 818-826. • International Conference 2. Phan Thi Dang Thu, Phan Dinh Huan and Nguyen Thanh Truong “Effect parametric to properties of a 2D orthogonal plain classical woven fabric composite”. International Conferrence on Engineering Mechanics and Automation (ICEMA), Ha Noi city 2014 - ISBN: 978-604-913-367-1, pages 509-517. • National Conference 3. Phan Thi Dang Thu, Phan Dinh Huan and Nguyen Thanh Truong “Biaxial beam inflation test on orthotropic fabric beam”; National Conference on Solid Mechanics, Ho Chi Minh city 2013 - ISBN: 978-604-913-213-1, pages 1169-1176. 4. Nguyen Thanh Truong, Phan Dinh Huan, Phan Thi Dang Thu “Discretizing an analytical inflating beam model by the shellmembrane finite elelment”. National Conference on Solid Mechanics, Ho Chi Minh city 2013 - ISBN: 978-604-913-213-1, pages 1221-1228. 5. Phan Thi Dang Thu, Le Manh Tuan, Nguyen Xuan Hung, Nguyen Thanh Truong “Geometrically nonlinear behaviour of composite beams of variable fiber volume fraction in isogeometric analysis”. National Conference on Solid Mechanics, Da Nang city 2015 - ISBN: 978-604-82-2028-0, Pages: 1404-1409. 6. Thu Phan-Thi-Dang, Tuan Le-Manh, Giang Le-Hieu, Truong Nguyen- Thanh “Buckling of cylindrical inflating composite beams using isogeometric analysis”. Proceedings of the National Conference on science and technology in List of publications 165 mechanics IV, Ho Chi Minh City 2015, Viet Nam - ISBN: 978-604-73-3691-3, Pages 821-826. 7. Phan Thi Dang Thu, Nguyen Thanh Truong, Phan Dinh Huan “Mô hình dầm hơi composite phi tuyến chịu uốn”. National Scientific Conference on Composite Materials and Structures, Nha Trang city 2016 - ISBN: 976-604-82-2026-6, Page 699-706. 8. Phan Thi Dang Thu, Nguyen Thanh Truong, Phan Dinh Huan, Le Dinh Tuan “Biaxial experiments for determining material properties and joint strength of textile plain woven fabric composites”. National Conference on Solid Mechanics, Ha Noi city 2017 - ISBN: 978-604-913-722-8, Page 1174-11.
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