Agile Wing Integration - Nonlinear devices on a strut for loads control

Research output

Research output per year 2016 2016 2017 2018 2019 2019

• 3 Conference Contribution (Conference Proceeding)
• 1 Article (Academic Journal)

Research output per year

Research output per year

Search results

• 2019

  Passive Gust Loads Alleviation in a Truss-Braced Wing Using an Inerter-Based Device

  Szczyglowski, C. P., Neild, S. A., Titurus, B., Jiang, J. Z. & Coetzee, E., 2019, In: Journal of Aircraft. 12 p.

  Research output: Contribution to journal › Article (Academic Journal) › peer-review

  Open Access

  File

  • Gust Loads 100%
  • Aerospace Applications 50%
  • Damping Coefficient 50%
  • Peak Load 50%
  13 Citations (Scopus)

  416 Downloads (Pure)