Help ?

IGMIN: あなたがここにいてくれて嬉しいです. お願いクリック '新しいクエリを作成してください' 当ウェブサイトへの初めてのご訪問で、さらに情報が必要な場合は.

すでに私たちのネットワークのメンバーで、すでに提出した質問に関する進展を追跡する必要がある場合は, クリック '私のクエリに連れて行ってください.'

Rare Disorders Brain Disorders Environmental Sciences Rehabilitation Sensors Sleep Disorders Physical Therapy Data Engineering Mycology Parasitology Urology Ecotoxicology Community Health Electronics Neurosurgery Public Health Sustainability Hematology Endocrinology Natural Resource Management
    

Focusing on Biology, Medicine and Engineering ISSN: 2995-8067 | Quick Google Scholar

Search
Organised by  IgMin Fevicon
Submit Manuscript

Subjects/Topics

Welcome to IgMin Research – an Open Access journal uniting Biology Group, Medicine Group, and Engineering Group. We’re dedicated to advancing global knowledge and fostering collaboration across scientific fields.

Biology Group
Medicine Group
Engineering Group
General Science Group
A to Z Topics

Members

Our mission is to promote a culture of collaborative thinking that drives faster advancements.

Editors
Authors
Submit Manuscript

Articles

Our mission is to promote a culture of collaborative thinking that drives faster advancements.

Early Online
Current Issue
Previous Issue
Archive
Browse by Universities
Table of Content

Explore Content

Our mission is to promote a culture of collaborative thinking that drives faster advancements.

Identify Us

Publish Now

Policies

Manuscript Guidelines

Other Services

Identify Us

Our mission is to promote a culture of collaborative thinking that drives faster advancements.

About Us
Contact us
Testimonials
IgMin Corporation

Welcome to IgMin, a leading platform dedicated to enhancing knowledge dissemination and professional growth across multiple fields of science, technology, and the humanities. We believe in the power of open access, collaboration, and innovation. Our goal is to provide individuals and organizations with the tools they need to succeed in the global knowledge economy.

Publications Support
publications.support@igmin.org
E-Books Support
ebooks.support@igmin.org
Webinars & Conferences Support
webinarsandconference@igmin.org
Content Writing Support
contentwriting.support@igmin.org
IT Support
it.support@igmin.org
IgMin Youtube Link

Search

Explore Section

Content for the explore section slider goes here.

79 of 162
Prevalence of Diabetic Retinopathy among Self-reported Newly Diagnosed Diabetics
Shweta Walia
81 of 162
AFM Analysis of Polymeric Membranes Fouling
Gordano A
Abstract

要約 at IgMin Research

Our mission is to promote a culture of collaborative thinking that drives faster advancements.

Engineering Group Research Article 記事ID: igmin191

Integrated Multi-fidelity Structural Optimization for UAV Wings

Materials Science DOI10.61927/igmin191
Sanusi Muhammad Babansoro * ,
Deng Zhongmin ,
Hasan Mehedi and
SM Tarikul Islam
Affiliation

Affiliation

    Sanusi Muhammad Babansoro, Beihang University, School of Astronautical Science and Engineering, Beijing 100083, China, Email: sanusimbabansoro@gmail.com

Fulltext HTML Fulltext PDF Cite this article
0
REFERENCES
2.0k
VIEWS
228
DOWNLOADS
93
Similar Articles
Connect with Us

要約

The paper explores comprehensive Unmanned Aerial Vehicle (UAV) wing optimization, integrating aerodynamic and structural techniques. A detailed comparison between the base and optimized modules while considering specifications such as composite material orientation, spar and rib material, deformation, stress, strain, safety factor, and weight. The methodology utilizes material changes for wing weight reduction while maintaining structural integrity. The optimized module (Case 7) balances weight reduction, safety, and structural performance, notably shifting from Al 7075 to Al 2024. Structural optimization focuses on changes in Carbon Fiber/Epoxy orientation, leveraging material changes for weight reduction. Constitutive equations and transformation matrices calculate stiffness matrices for the laminate, resulting in a robust wing. This holistic optimization combines low and high-fidelity techniques, addressing UAV wing structural aspects. Outcomes include weight reduction, deformation minimization, fluttering modal deformation and buckling points, an increased factor of safety, and improved strength-to-weight ratio. The research significantly advances aerospace engineering, particularly in UAV design and optimization.

数字

Methodology Demonstration. Figure 1: Methodology Demonstration....
Structural Methodology Application Flowchart. Figure 2: Structural Methodology Application Flowchart....
Computational Stiffness Value for 6-Layer Configuration. Figure 3: Computational Stiffness Value for 6-Layer Configur...
Flow Chart for Aero-Structural Analysis. Figure 4: Flow Chart for Aero-Structural Analysis....
Rib and Spar Meshing on Mechanical Design. Figure 5: Rib and Spar Meshing on Mechanical Design....
Skin Coupled Meshing for Skin, Rib, and Spar. Figure 6: Skin Coupled Meshing for Skin, Rib, and Spar....
Pressure load distribution along the wing's lower surface. Figure 7: Pressure load distribution along the wing's lower ...
Pressure load distribution along the wing upper surface. Figure 8: Pressure load distribution along the wing upper su...
Structural Analysis and Optimization 1 Flowchart. Figure 9: Structural Analysis and Optimization 1 Flowchart....
Fluttering Modes EGlass/Epoxy. Figure 10: Fluttering Modes EGlass/Epoxy....
Buckling EGlass/Epoxy. Figure 11: Buckling EGlass/Epoxy....
Fluttering SGlass/Epoxy. Figure 12: Fluttering SGlass/Epoxy....
Buckling SGlass/Epoxy. Figure 13: Buckling SGlass/Epoxy....
Fluttering Modes Carbon Fibre/Epoxy. Figure 14: Fluttering Modes Carbon Fibre/Epoxy....
Buckling Epoxy Carbon Fibre. Figure 15: Buckling Epoxy Carbon Fibre....
Deformation Static Optimized Wing 1. Figure 16: Deformation Static Optimized Wing 1....
Strain Static Optimized Wing 1. Figure 17: Strain Static Optimized Wing 1....
Stress Static Optimized Wing 1. Figure 18: Stress Static Optimized Wing 1....
Fluttering Mode 1. Figure 19: Fluttering Mode 1....
Fluttering Mode 2. Figure 20: Fluttering Mode 2....

参考文献

    1. Hua S, Liangxian G, Chunlin G. CST Research on Geometry Modeling Method Based on Three-dimensional CST Parameterization Technology. International Journal of Aerospace Engineering. 2021; 56(2): 211-342.
    2. Berci M, Toropov V V, Hewson R W. Meta modelling based on High and Low Fidelity Models Interaction for UAV Gust Performance Optimization. Journal of Mechanical Engineering Science. 2012; 54(4): 409-435
    3. Kurt H B, Millidere M, Gomec FS. Multi-fidelity Aerodynamic Dataset Generation of a Fighter Aircraft[J]. Turkish Aerospace, Ankara, Turkey. Middle East Technical University, Ankara, Turkey. 2021; 3007.
    4. Berci M, Toropov VV, Hewson RW. Multidisciplinary Multifidelity Optimisation of a Flexible Wing Aerofoil for Small UAV[D]. School of Mechanical Engineering, University of Leeds, Leeds, LS2 9JT, UK, 2018; 76: 5(3).
    5. Trad H, Segui M, Botez RM. Airfoils Generation Using Neural Networks, CST Curves and Aerodynamic Coefficients. AIAA. 2020; 2514(6): 2020-2773.
    6. Gidudu A, Hulley G, Marwala T. Classification of Images Using Support Vector Machines. Department of Electrical and Information Engineering, University of the Witwatersrand, Johannesburg, Private Bag X3, Wits, South Africa. 2018; 3007.
    7. Hu MY, Xiangming Z, Bo Z. Theoretical Calculation of Stiffness of Composite Laminated Beam with T-Section. International Conference on Structural, Mechanical and Materials Engineering (ICSMME). 2015; 5400.
    8. Masters DA, Taylor NJ, Rendall TC. A geometric comparison of aerofoil shape parameterisation methods. AIAA Journal. Advance online publication. 2017; 2773.
    9. Mitchell TA, Jacob JD. Evaluation of Bird-Wing-Inspired Features on Biomimetic UAVs. 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. 2013; 0709-3967.
    10. Fajar A. W, Mohammad A. The maritime surveillance unmanned aerial vehicle. AIP Conference Proceedings. 2020; 2227: 020029.
    11. Marta A, Muis A. Flight Dynamics Modeling of Dual Thrust System Hybrid UAV[C]. International Conference on Artificial Intelligence and Mechatronics Systems (AIMS), Bandung, Indonesia. 2021; 147-150.
    12. Andrew TR, Hua S, Richard B. Damage Resistance and Damage Tolerance of Hybrid Carbon-Glass Laminates. 52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Denver, Colorado. 2011; 55(5): 1575-1589.
    13. Avinash B, Kumar SA, Krishna VC. Conceptual Design of Hybrid UAV. International Journal of Engineering Research & Technology (IJERT). 2015; 4(12): 89.
    14. Natsuki T, Kenichi S. Structural and Aeroelastic Studies of Wing Model for Transonic Wind Tunnel Test Fabricated by Additive Manufacturing with AlSi10Mg Alloys. Chicago, IL & Virtual. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. AIAA SciTech Forum. 2022; 45(2): 53-69.
    15. Sanchez RLM, Lozano R, Arias A. Development, Modeling and Control of a Dual Tilt-Wing UAV in Vertical Flight. Drones, Hal Open Science Journal. 2020; 71(4): 26-32.
    16. Spar PM, Thiago RC, Eduardo CS. Design and Manufacturing Process of a UAV Composite Wing. 4th Brazilian Conference on Composite Materials, Rio de Janeiro, 2018; 3418.
    17. Lapan M.M. LSU-02 NGLD: The Latest Generation of Maritime Reconnaissance Drones, Longer Roaming Range. Asia-Pacific International Symposium on Aerospace Technology Tokyo. 2013; 4(4):71.
    18. Sigmund O. Design of Multiphysics Actuators Using Topology Optimization; One Material Structures. Computer methods in Applied Mechanics and Engineering. 2001; 190(49): 6577.
    19. Syafrina SK, Gaguk M, Farid J, Arifin RS. Aerodynamic Analysis of Additional Winglet on LSU-02 Ngld Aircraft Wings with Canted Angle Variations. 2021; 7(2): 247-254.
    20. Nur MU, Aryandi M, Yusuf GW. Wing Static Test of LSU-02 NGLD Aircraft Using Whiffletree Method. AIP Conf Proc. 2019: 2088(1).
    21. Black C, Singh KV, Goodman S. et al. Design, fabrication and testing of 3D printed wings for rapid evaluation of aeroelastic performance. AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. 1997; 2018. 1997
    22. Locascio DB, Ramee CL, Cooksey KD. A framework for integrated analysis, design, and rapid prototyping of small unmanned airplanes. 16th AIAA Aviation Technology, Integration, and Operations Conference. 2016; 3447.
    23. Mariens J. Wing Shape Multidisciplinary Design Optimization Master's thesis. Delft University of Technology. 2012; 24(6): 709-719.
    24. Moraira H. Study and Structural Analysis of a Monocoque Wing with Composite Materials for a Model Aircraft (Bachelor’s degree thesis. Bachelor’s degree in Aerospace Vehicles Engineering, Universitat Politècnica de Catalunya, Escola Superior d’Enginyeries Industrial, Aeroespacial i Audiovisual de Terrassa, 2017.
    25. Cal M. Preliminary Topology Optimization of Small Unmanned Aircraft Wings for Additive Manufacturing Dissertation for obtaining the Master's Degree in Aerospace Engineering, integrated study cycle. Covilhã, 2019.
    26. Rosenbaum EB, Mikkelsen TQ. Hybrid Wing Body Aircraft Concepts and Aerodynamics. Aerospace Engineering, University of Maryland, College Park, Maryland, 2017.
    27. Peng W, Kun Z, Chao Z. Design and analysis of aerodynamics for an unmanned aerial vehicle (UAV) for surveillance application[J]. American Journal of Physics. 2016; 33: 49-54.
    28. Gardan J. Additive manufacturing technologies: State of the art and trends. International Journal of Production Research. 2016; 54(10): 3118–3132.
    29. Li S, Liu Y, Jiang Z, Hu G, Noack B R. Raps F. Aerodynamic Characterization of a Fan-Array Wind Generator[J]. American Institute of Aeronautics and Astronautics, Published online. 2023; 33(9): 1746-1754.
    30. Clarendon, Indoor Environmental Quality in Air-conditioned Mosque Buildings in Kuwait. American Journal of Civil Engineering and Architecture. 2017: 68–73.
    31. Obert E. Aerodynamic Design of Transport Aircraft. Amsterdam: IOS Press, Delft University Press. 2009.
    32. Vani PS, Reddy DV, Prasad BS. Design and Analysis of A320 Wing using E-Glass Epoxy Composite. International Journal of Engineering Research & Technology. 2014; 536–539.
    33. Raymer DP. Aircraft Design, A Conceptual Approach Second Edition. Washington, DC, American Institute of Aeronautics and Astronautics, Inc., 1992.
    34. Karukana CS. Study of Flow Field over Fabricated Airfoil Models of NACA 23015 with its Kline-Fogelman Variant. Advances in Aerospace Science and Application. 2013; 3(2):95-100.
    35. Anderson JD. Introduction to Flight 7th Edition. McGraw-Hill. 2012.
    36. Abduljalil MH, Kuntjoro W, Mahmud J. Wing structure static analysis using super Element. Procedia Engineering. 2012; 41: 1600–1606.
    37. Baughn TV, Packman PF. Finite element analysis of an ultra-light aircraft. Journal of Aircraft. 1986; 23:82-86.
    38. Yuvraj SR, Subramanyam P. Design and analysis of Wing of an ultra-light Aircraft. International Journal of Innovative Research in Science, Engineering and Technology. 2015; 4:78-85.
    39. Anderson J D. Introduction to Flight 6th Edition. Curator of Aerodynamics National Air and Space Museum Smithsonian Institution and Professor Emeritus University of Maryland, 2017.
    40. Bruhn EF. Analysis and Design of Flight Vehicle Design 1st Edition. 2005.
    41. Raymer DP. Aircraft Conceptual Design 2nd Edition. Hugh Nelson, Aero Engineering. Part I, George Newnes[M]. 1938; 2.
    42. Srinadh B, Devika S. Computational Study on Supercritical Airfoil. 1992.
    43. Wang K. Vibration Analysis OF Cracked Composite Bending Torsion Beams for Damage Diagnosis. 2004.
    44. Stegmmann J. Analysis and Optimization of Laminated Composite Shell Structure. Structural and Multidisciplinary Optimization. 2005; 29(5):349-360.
    45. Hiro M. Development of a Composite Tailoring Technique for Airplane Wing. 1996; 1(26):205326.
    46. Guo SJ, Bannerjee JR, Cheung CW. The Effect of Laminate Lay-Up on the Flutter Speed of Composite Wings. Journal of Aerospace Engineering. 2002; 217(3):115-122.
    47. Development of a Composite Tailoring Procedure for Airplane Wing. 2005.
    48. Shyama K, Sinha PK. Finite Element Analysis of Composite Wing TJoints. 2002.
    49. Alastair FJ, Nathalie P. Modeling Impact Damage in Double-Walled Composite Structures. 2005.
    50. Boyang L. Two-Level Optimization of Composite Wing Structure Based on Panel Genetic Optimization. 2001.
    51. Benini GR, Belo EM, Marques FD. Numerical Model for the Simulation of Fixed Wings Aeroelastic Response. 2004.
    52. Seong WH, Byung SK, Joong YP. Dynamic Analysis of Bending-Torsion Coupled Beam Structures Using Exact Dynamic Elements. 2003.
    53. Pawara PB, Abhay A. Analysis of Composite Material aircraft wing under Static Loading Condition. International Journal of Engineering Development and Research conference session. 2017.
    54. Bogdan C, Dorin L, Radu B. Stress and Modal Analysis Report for Avert Program. 2009.
    55. Rajappan R, Pugazhenthi V. Finite Element Analysis of Aircraft Wing Using Composite Structure. 2013.
    56. Prabhu NR, Ramesh CS, Chandrashekar T. Effect of Heat Treatment on Strength and Abrasive Wear Behavior of Al6061–SiCp Composites. 2010; 33:49-54.
    57. Anderson JD. Introduction to Flight, fifth edition, The McGraw-Hill companies. 2007.
    58. Jan R, Chuan T. Airplane Aerodynamics and Performance. 1997
    59. Xi P, Zhang BY, Ning T. Intelligent Product Design Based on Open Knowledge Representation. 2012; 33(9):1746-1754.
    60. Anemaat WA, Schueler KL. Airplane Layout Design Using Object Oriented Methods. 1997; 5510.
    61. Feng HC, Luo MQ, Liu H. Knowledge-Based and Extensible Aircraft Conceptual Design Environment. 2011; 24(6): 709-719
    62. La RG, Tooren MJL. Knowledge-Based Engineering Approach to Support Aircraft Multidisciplinary Design and Optimization. 2009; 46(6): 1875-1885.
    63. Sears FW. An Introduction to Thermodynamics. The Kinetic Theory of Gases, and Statistical Mechanics, 2d ed., Addison-Wesley Publishing Company, Inc. Reading. Mass. 1959; 28: 23-50.
    64. Wylen VGJ, Sonntag RE. Fundamentals of Classical Thermodynamics. 2d ed., John Wiley & Sons, Inc., New York. 1973; 53-88.
    65. Reynolds WC, Perkins HC. Engineering Thermodynamics. 2d ed., McGraw-Hill Book Company, New York. 1977.
    66. Shapiro AH. The Dynamics and Thermodynamics of Compressible Fluid Flow. vols. 1 and 2, The Ronald Press Company, New York. 1953.
    67. Leipmann HW, Roshko A. Elements of Gas dynamics[M]. John Wiley & Sons, Inc., New York. 1957.
    68. Tsien HS. Two-Dimensional Subsonic flow of Compressible Fluids. J. Aeronaut. Sci. 10 October 1939: 6-399.
    69. Karman VTH. Compressibility Effects in Aerodynamics[J]. Aeronaut. Sci. 2012; 8(9): 992-1011.
    70. Laitone EV. New Compressibility Correction for Two-Dimensional Subsonic Flow[J]. J. Aeronaut. Sci, 2012; 18(5): 350-350.
    71. Whitcomb RT. A Study of the Zero-Lift Drag-Rise Characteristics of Wing-Body Combinations Near the Speed of Sound. NACA 1273 report. 1956.
    72. Whitcomb RT, Clark LR. An Airfoil Shape for Efficient Flight at Supercritical Mach Numbers. NASA TMX-1109, July 1965.
    73. Owczarek JA. Fundamental of Gas Dynamics. International Textbook Company, Scranton. Pa. 1964.
    74. Anderson JD, Albacete L M, Winkelmann AE. On Hypersonic Blunt Body Flow Fields Obtained with a Time-Dependent Technique. Naval Ordnance Laboratory NOLTR. 1968; 68-129.
    75. Anderson JD. An Engineering Survey of Radiating Shock Layers. AIAA, September, 1969; 7(9): 1665–1675.
    76. Cherni GG. Introduction to Hypersonic Flow. Journal of the Aeronautical Sciences. 191: 18(5):350-350.

類似の記事

Revisiting Ice Ages Cycles
Donald Rapp
DOI10.61927/igmin239
The Influence of Low Pesticide Doses on Fusarium Molds
Mihaela Ursan, Oana-Alina Boiu-Sicuia, Ioana Irina Crăinescu and Călina Petruța Cornea
DOI10.61927/igmin226
Cyber Threat Analysis (CTA) in Current Conflicts
Zbigniew Ciekanowski and Sławomir Żurawski
DOI10.61927/igmin169
The Expressivity Dimension of Speech is the basis of the Expression Dimension. Evidence from Behavioural and Neuroimaging Studies
Isabelle Hesling
DOI10.61927/igmin182
Educational Innovation amidst Globalization: Higher Education Institutions and Societal Integration
Zainab Rasheed
DOI10.61927/igmin131
Lifestyle and Well-being among Portuguese Firefighters
Laura Carmona, Raquel Pinheiro, Joana Faria-Anjos, Sónia Namorado and Maria José Chambel
DOI10.61927/igmin146
Issues of Manufacturability of Roller Machines
Ayder Nabiev and Khushnudbek Rakhmonov
DOI10.61927/igmin252
Prevalence of Non-specific Low Back Pain Among Chinese Healthcare Workers (Surgeons and Surgical Nurses): A Multi-Center Survey Study
Jamal Alshorman, Ruba Altahla, Ahmad Alkhatatbeh, Wan Li and Feronika Prabowo
DOI10.61927/igmin264
On how Doping with Atoms of Gadolinium and Scandium affects the Surface Structure of Silicon
Egamberdiev BE, Daliev Kh S, Khamidjonov I Kh, Norkulov Sh B and Erugliev UK
DOI10.61927/igmin206
The Examination of Game Skills of Children Aged 5-6 Years Participating in Movement Education
Bekir Erhan Orhan, Aydin Karaçam and Yuni Astuti
DOI10.61927/igmin196
Page Navigation
タイトルと著者 要約 数字 参考文献 類似の記事 View PDF
研究を公開する

私たちは、科学、技術、工学、医学に関する幅広い種類の記事を編集上の偏見なく公開しています。

提出する

見る 原稿のガイドライン 追加 論文処理料

IgMin 科目を探索する
Biology Medicine Engineering General Science

現在トレンドになっている記事はどれですか？

トップ10の記事をクリック

クイックリンク

原稿を提出する
IgMinリサーチを購読する

発表された記事、号のリリース、ジャーナル活動の最新情報についてのお知らせを受け取るために、メールアドレスを入力してください。

研究論文
  1. Technical & Economic Feasibility Study of Proposed Pump Storage Power Plants at Kuda Oya, Mul Oya, Gurugal Oya, and Dambagasthalawa
  2. Cyber Threat Analysis (CTA) in Current Conflicts
  3. Study of the Histological Features of the Stroma of High-Grade Gliomas Depending on the Status of the Mutation in the IDH1 Gene
  4. EB Naevi-like Lesion in Infant Bullous Pemphigoid
  5. Prevalence of Diabetic Retinopathy among Self-reported Newly Diagnosed Diabetics
  6. Designing a Compact High-precision Positioner with Large Stroke Capability for Nanoindentation Devices
もっと読む
グーグルスカラー
welcome Image

Google Scholarは2004年11月にベータ版が発表され、幅広い学術領域を航海する学術ナビゲーターとして機能します。それは査読付きジャーナル、書籍、会議論文、論文、博士論文、プレプリント、要約、技術報告書、裁判所の意見、特許をカバーしています。 IgMin の記事を検索