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Development of analytical method for structural design of morphing wings with corrugated structures

Research Project

Project/Area Number 15K06598
Research Category

Grant-in-Aid for Scientific Research (C)

Allocation TypeMulti-year Fund
Section一般
Research Field Aerospace engineering
Research InstitutionThe University of Tokyo

Principal Investigator

Yokozeki Tomohiro  東京大学, 大学院工学系研究科(工学部), 准教授 (50399549)

Project Period (FY) 2015-04-01 – 2018-03-31
Project Status Completed (Fiscal Year 2017)
Budget Amount *help
¥4,680,000 (Direct Cost: ¥3,600,000、Indirect Cost: ¥1,080,000)
Fiscal Year 2017: ¥2,600,000 (Direct Cost: ¥2,000,000、Indirect Cost: ¥600,000)
Fiscal Year 2016: ¥1,170,000 (Direct Cost: ¥900,000、Indirect Cost: ¥270,000)
Fiscal Year 2015: ¥910,000 (Direct Cost: ¥700,000、Indirect Cost: ¥210,000)
Keywords航空宇宙工学 / 構造・材料 / 可変翼構造 / 航空機 / 空力特性 / 構造解析
Outline of Final Research Achievements

This study aimed to develop the structural design methodology for morphing wings with corrugated structures as a candidate for the variable camber morphing wing. A simplified structural analysis considering large deformation and an aerodynamic analysis are combined to estimate the optimal deformation for morphing wings with actuation mechanisms. Optimization has been conducted for better aerodynamic performance by changing structural parameters of corrugated structures.

Report

(4 results)
  • 2017 Annual Research Report   Final Research Report ( PDF )
  • 2016 Research-status Report
  • 2015 Research-status Report
  • Research Products

    (9 results)

All 2017 2016 2015

All Journal Article (3 results) (of which Peer Reviewed: 3 results,  Open Access: 2 results,  Acknowledgement Compliant: 1 results) Presentation (6 results) (of which Int'l Joint Research: 5 results)

  • [Journal Article] Aero-Structural Evaluation of Morphing Control Surface Using Corrugated Panels2017

    • Author(s)
      K. Sato、 T. Yokozeki
    • Journal Title

      TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN

      Volume: 15 Issue: APISAT-2016 Pages: a7-a15

    • DOI

      10.2322/tastj.15.a7

    • NAID

      130005868617

    • ISSN
      1884-0485
    • Related Report
      2017 Annual Research Report
    • Peer Reviewed / Open Access
  • [Journal Article] Fundamental Study on Adaptive Wing Structure for Control of Wing Load Distribution2017

    • Author(s)
      K. Fujii、 T. Yokozeki、 H. Arizono、 M. Tamayama
    • Journal Title

      TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN

      Volume: 15 Issue: APISAT-2016 Pages: a83-a88

    • DOI

      10.2322/tastj.15.a83

    • NAID

      130006191043

    • ISSN
      1884-0485
    • Related Report
      2017 Annual Research Report
    • Peer Reviewed / Open Access
  • [Journal Article] Development of variable camber wing with morphing leading and trailing sections using corrugated structures2016

    • Author(s)
      H. Takahashi, T. Yokozeki, Y. Hirano
    • Journal Title

      Journal of Intelligent Material Systems and Structures

      Volume: 27 Issue: 20 Pages: 2827-2836

    • DOI

      10.1177/1045389x16642298

    • Related Report
      2016 Research-status Report
    • Peer Reviewed / Acknowledgement Compliant
  • [Presentation] Study adaptive wing structure for compromising structural strength and aerodynamic performance2017

    • Author(s)
      M. Tamayama, K. Fujii, T. Yokozeki, H. Arizono
    • Organizer
      International Forum on Aeroelasticity and Structural Dynamics 2017
    • Related Report
      2017 Annual Research Report
    • Int'l Joint Research
  • [Presentation] Aero-structural evaluation of morphing control surface using corrugated panels2016

    • Author(s)
      K. Sato, T. Yokozeki
    • Organizer
      The 2016 Asia-Pacific International Symposium on Aerospace Technology
    • Place of Presentation
      Toyama
    • Year and Date
      2016-10-25
    • Related Report
      2016 Research-status Report
    • Int'l Joint Research
  • [Presentation] Fundamental study on adaptive wing structure for control of wing load distribution2016

    • Author(s)
      K. Fujii, T. Yokozeki, H. Arizono, M. Tamayama
    • Organizer
      The 2016 Asia-Pacific International Symposium on Aerospace Technology
    • Place of Presentation
      Toyama
    • Year and Date
      2016-10-25
    • Related Report
      2016 Research-status Report
    • Int'l Joint Research
  • [Presentation] Structural design of morphing control surface using corrugated panels2016

    • Author(s)
      K. Sato, T. Yokozeki
    • Organizer
      First International Symposium on Flutter and its Application
    • Place of Presentation
      Tokyo
    • Year and Date
      2016-05-16
    • Related Report
      2016 Research-status Report
    • Int'l Joint Research
  • [Presentation] コルゲート構造を用いたキャンバーモーフィング翼の構造解析評価2016

    • Author(s)
      佐藤圭悟、横関智弘
    • Organizer
      第58回構造強度に関する講演会
    • Place of Presentation
      札幌
    • Related Report
      2016 Research-status Report
  • [Presentation] Variable Camber Morphing Wing Using Corrugated Structures2015

    • Author(s)
      Tomohiro Yokozeki, Hiroki Takahashi, Yoshiyasu Hirano
    • Organizer
      26th International Conference on Adaptive Structures and Technologies
    • Place of Presentation
      神戸ファッションマート(兵庫県、神戸市)
    • Year and Date
      2015-10-13
    • Related Report
      2015 Research-status Report
    • Int'l Joint Research

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Published: 2015-04-16   Modified: 2019-03-29  

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