Open Access
Issue
JNWPU
Volume 41, Number 2, April 2023
Page(s) 329 - 337
DOI https://doi.org/10.1051/jnwpu/20234120329
Published online 07 June 2023
  1. YOKOZEKI T, TAKEDA S, OGASWARA T, et al. Mechanical properties of corrugated composites for candidate materials of flexible wing structures[J]. Composites Part A: Applied Science and Manufacturing, 2006, 37(10): 1578–1586 [Article] [Google Scholar]
  2. BAI J B, CHEN D, XIONG J J, et al. A corrugated flexible composite skin for morphing applications[J]. Composites Part B Engineering, 2017, 131134–143 [Article] [CrossRef] [Google Scholar]
  3. ZHAO J T, WANG B F, MOU C W, et al. Research on tensile deformation and strain of composite corrugated skin[J]. China Mechanical Engineering, 2010, 21(16): 1959–1962 [Google Scholar]
  4. MOU C W, WANG B F, GE R J, et al. Basal body preparation and drive characteristic of corrugated skin with the active deformability[J]. Ordnance Material Science and Engineering, 2010, 32(2): 11–14 [Google Scholar]
  5. OLYMPIO K R, GANDHI F. Flexible skins for morphing aircraft using cellular honeycomb cores[J]. Journal of Intelligent Material Systems & Structures, 2010, 21(17): 1719–1735 [Google Scholar]
  6. BUBERT E A, WOODS B, LEE K, et al. Design and fabrication of a passive 1D morphing mircraft skin[J]. Journal of Intelligent Material Systems & Structures, 2010, 21(17): 1699–1717 [Google Scholar]
  7. GONG Xiaobo. Research on variable camber wing structure based on variable stiffness skin and zero Poisson′s ratio honeycomb[D]. Harbin: Harbin Institute of Technology, 2017 (in Chinese) [Google Scholar]
  8. KUDVA J N, SANDERS B P, PINKERTON-FLORANCE J L, et al. Overview of the DARPA/AFRL/NASA smart wing phase Ⅱ program[C]//Smart Structures and Materials 2001: Industrial and Commercial Applications of Smart Structures Technologies, 2001: 383–389 [Google Scholar]
  9. SUN J, GONG X, LIU Y, et al. Variable camber wing based on shape memory polymer skin[C]//54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2013: 1919 [Google Scholar]
  10. CHEN S B, CHEN Y J, ZHANG Z C, et al. Experiment and analysis of morphing skin embedded with shape memory polymer composite tube[J]. Journal of Intelligent Material Systems and Structures, 2014, 25(16): 2052–2059 [Article] [CrossRef] [Google Scholar]
  11. MURRAY G, GANDHI F, BAKIS C. Flexible matrix composite skins for one-dimensional wing morphing[J]. Journal of Intelligent Material Systems & Structures, 2010, 21(17): 1771–1781 [Google Scholar]
  12. TIMOSHENKO S P. On the correction for shear of the differential equation for transverse vibrations of prismatic bars[J]. The London, Edinburgh, and Dusblin Philosophical Magazine and Journal of Science, 1921, 41(245): 744–746 [Article] [CrossRef] [Google Scholar]
  13. ZHANG Hongzhi. Topological optimization design of trailing edge of segmented variable camber wing[D]. Xi′an: Northwestern Polytechnical University, 2021 (in Chinese) [Google Scholar]

Current usage metrics show cumulative count of Article Views (full-text article views including HTML views, PDF and ePub downloads, according to the available data) and Abstracts Views on Vision4Press platform.

Data correspond to usage on the plateform after 2015. The current usage metrics is available 48-96 hours after online publication and is updated daily on week days.

Initial download of the metrics may take a while.