New concept "local joint coordinates" to break down the barrier of flexible deployable wing model between 2-D and 3-D dimensions

• Project/Area Number: 18K18905
• Research Category: Grant-in-Aid for Challenging Research (Exploratory)
• Allocation Type: Multi-year Fund
• Review Section: Medium-sized Section 24:Aerospace engineering, marine and maritime engineering, and related fields
• Research Institution: Tohoku University
• Principal Investigator: MAKIHARA Kanjuro 東北大学, 工学研究科, 教授 (60392817)
• Co-Investigator(Kenkyū-buntansha): 亀山 正樹 信州大学, 学術研究院工学系, 准教授 (30302178) ; 永井 大樹 東北大学, 流体科学研究所, 教授 (70360724)
• Project Period (FY): 2018-06-29 – 2020-03-31
• Project Status: Completed (Fiscal Year 2019)
• Budget Amount: ¥6,240,000 (Direct Cost: ¥4,800,000、Indirect Cost: ¥1,440,000); Fiscal Year 2019: ¥1,950,000 (Direct Cost: ¥1,500,000、Indirect Cost: ¥450,000); Fiscal Year 2018: ¥4,290,000 (Direct Cost: ¥3,300,000、Indirect Cost: ¥990,000)
• Keywords: 局所ジョイント座標 / 柔軟展開翼 / 展開翼 / モデリング / 風洞実験 / 空力連成モデル

Outline of Final Research Achievements

This is a challenging study to extend a 2D flexible deployable wing model to a 3D model using a new concept [local joint coordinates]. It was conceived that by appropriately introducing "extension deformation small" based on the structural characteristics of flexible wings, it is possible to define [local joint coordinates] that can express the three-dimensional deployment angle. We challenged 3D structural modeling with this new idea. To create a realistic modeling method, we conducted a wind tunnel experiment considering three-dimensional effects.

Academic Significance and Societal Importance of the Research Achievements

挑戦的研究としての意義は，①提案する【局所ジョイント座標】により，従来不可能とされてきた「３次元運動する柔軟展開構造の展開角表現」と「空気力の作用方向の３次元定義」に挑戦する意義と，②提案する３次元モデル構築の精度を精査するために風洞実験での実証に挑戦する意義である．過去研究から得られる知見が圧倒的に乏しい未開拓研究領域で，国際協力と風洞実験を活用して構造モデルのみならず空力モデルも３次元へと到達しようとする挑戦的な意義を有する．

Research Products

• [Int'l Joint Research] University of Warwick(英国)
• [Int'l Joint Research] Imperial College London/University of Warwick(英国)
• [Journal Article] Absolute Nodal Coordinate Beam Element for Modeling Flexible and Deployable Aerospace Structures (2019)
  • Author(s): Otsuka, K., and Makihara, K.
  • Journal Title: AIAA Journal Volume: 57 Issue: 3 Pages: 1343-1346
  • DOI: 10.2514/1.j057780
  • Peer Reviewed
• [Journal Article] Geometrically nonlinear electro-aeroelastic framework for morphing wing with piezoelectric actuators (2019)
  • Author(s): TSUSHIMA Natsuki、ARIZONO Hitoshi、YOKOZEKI Tomohiro、MAKIHARA Kanjuro
  • Journal Title: Transactions of the JSME (in Japanese) Volume: 85 Issue: 878 Pages: 18-00506-18-00506
  • DOI: 10.1299/transjsme.18-00506
  • NAID: 130007733853
  • ISSN: 2187-9761
  • Peer Reviewed
• [Journal Article] Multifidelity Modeling of Deployable Wings: Multibody Dynamic Simulation and Wind Tunnel Experiment (2019)
  • Author(s): Otsuka Keisuke、Wang Yinan、Fujita Koji、Nagai Hiroki、Makihara Kanjuro
  • Journal Title: AIAA Journal Volume: 57 Issue: 10 Pages: 4300-4311
  • DOI: 10.2514/1.j058676
  • Int'l Joint Research
• [Journal Article] Deployment Simulation Using Absolute Nodal Coordinate Plate Element for Next-Generation Aerospace Structures (2018)
  • Author(s): Otsuka, K., and Makihara, K.
  • Journal Title: AIAA Journal Volume: 56 Issue: 3 Pages: 1266-1276
  • DOI: 10.2514/1.j056477
  • Peer Reviewed
• [Journal Article] Versatile Absolute Nodal Coordinate Formulation Model for Dynamic Folding Wing Deployment and Flutter Analyses (2018)
  • Author(s): Otsuka Keisuke、Wang Yinan、Makihara Kanjuro
  • Journal Title: Journal of Vibration and Acoustics Volume: 141 Issue: 1 Pages: 011014-011014
  • DOI: 10.1115/1.4041022
  • Peer Reviewed / Int'l Joint Research
• [Presentation] New Framework of Strain Based Beam Formulation for Rigid Body Motion (2019)
  • Author(s): Suzaki, T., Otsuka, K., Hirotani, S., Dong, S., and Makihara, K.
  • Organizer: 16th International Conference on Flow Dynamics
• [Presentation] Comparison of 2D and 3D Simulation Models for Deployable Wing (2019)
  • Author(s): Otsuka, K., Suzaki, T., Wang, Y., Fujita, K., Nagai, H., and Makihara, K.
  • Organizer: 19th International Symposium on Advanced Fluid Information
  • Int'l Joint Research
• [Presentation] Deployable Wing Model Using ANCF and UVLM: Multibody Dynamic Simulation and Wind Tunnel Experiment (2019)
  • Author(s): Otsuka, K., Wang, Y., Fujita, K., Nagai, H., and Makihara, K.
  • Organizer: AIAA Scitech 2020 Forum
  • Int'l Joint Research
• [Presentation] Strain Based Beam Formulationの発展手法に関する研究 (2019)
  • Author(s): 須崎貴大，大塚啓介，小貫慧，槙原幹十朗
  • Organizer: 日本機械学会東北支部第54期総会講演会
• [Presentation] 鳥の羽を模した折り畳み機構を有する翼のマルチボディ解析 (2019)
  • Author(s): 大塚啓介，須崎貴大，藤田昂志，永井大樹，槙原幹十朗
  • Organizer: 第57回飛行機シンポジウム
• [Presentation] 3Dプリンティング翼の空力弾性特性 (2019)
  • Author(s): 津島夏輝，玉山雅人，槙原幹十朗，有薗仁
  • Organizer: 第28回交通・物流部門大会
• [Presentation] ANCF-ICE Beam Element for Modeling Highly Flexible and Deployable Aerospace Structures (2019)
  • Author(s): Keisuke Otsuka, Kanjuro Makihara
  • Organizer: 2019 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
  • Int'l Joint Research
• [Presentation] Motion Analysis of Flexible Folding Wing with a Hinge Joint Loaded by Gust (2018)
  • Author(s): Satoru Onuki, Keisuke Otsuka, Takahiro Suzaki, Hiroki Nagai, Koji Fujita, Kanjuro Makihara
  • Organizer: 15th International Conference on Flow Dynamics
  • Int'l Joint Research
• [Presentation] Simulation and Control of Flexible Aero-Structures using Nonlinear Reduced-Order Models (2018)
  • Author(s): Yinan Wang, Keisuke Otsuka, Koji Fujita, Hiroki Nagai, Kanjuro Makihara
  • Organizer: 15th International Conference on Flow Dynamics
  • Int'l Joint Research
• [Presentation] Dynamic Simulation of Deployable Wing Mars Airplane (2018)
  • Author(s): Keisuke Otsuka, Yinan Wang, Koji Fujita, Hiroki Nagai, Kanjuro Makihara
  • Organizer: 18th International Symposium on Advanced Fluid Information
  • Int'l Joint Research
• [Presentation] 全体座標表現に基づく柔軟展開翼の３次元マルチボディ解析法の開発 (2018)
  • Author(s): 大塚啓介，槙原幹十朗
  • Organizer: 第60回構造強度に関する講演会
• [Presentation] 展開型モーフィング翼の柔軟マルチボディシミュレーション (2018)
  • Author(s): 大塚啓介，槙原幹十朗
  • Organizer: Dynamics and Design Conference 2018
• [Presentation] 歪量を要素変数とする３次元柔軟梁要素の研究 (2018)
  • Author(s): 須崎貴大，大塚啓介，小貫慧，槙原幹十朗
  • Organizer: 東北支部第54期秋季講演会
• [Presentation] ピエゾアクチュエータによるモーフィング翼の非線形空力弾性解析 (2018)
  • Author(s): 津島夏輝，有薗仁，横関智弘，槙原幹十朗
  • Organizer: 第27回交通・物流部門大会