ALPES

  • Castellani, Michele (Researcher)
  • Castrichini, Andrea (Researcher)
  • Gaitonde, Ann L (Co-Principal Investigator)
  • Jones, Dorian P (Co-Principal Investigator)
  • Lowenberg , Mark H (Co-Principal Investigator)
  • Poncet-Montanges, A P (Researcher)
  • Tartaruga, Irene (Researcher)
  • Valente, Carmine (Researcher)
  • Cooper, Jonathan E (Principal Investigator)

Project Details

Description

Aircraft Loads Prediction using Enhanced Simulation (ALPES) is an EC FP7 Marie Curie European Industrial Doctorate Training Network. The aim of the network is to improve the prediction accuracy and efficiency of the loads experienced by an aircraft in-flight and on the ground.

The ALPES network involves five PhDs combining a novel research programme with a highly industrially focused training schedule, including placements at Airbus in the UK and/or France.
StatusFinished
Effective start/end date1/10/1330/09/17

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  • Research Output

    • 10 Article (Academic Journal)
    • 4 Conference Contribution (Conference Proceeding)
    • 1 Conference Paper

    Nonlinear Negative Stiffness Wingtip Spring Device for Gust Loads Alleviation

    Castrichini, A., Cooper, J. E., Wilson, T., Carrella, A. & Lemmens, Y., Mar 2017, In : Journal of Aircraft. 54, 2, p. 627-641 15 p.

    Research output: Contribution to journalArticle (Academic Journal)

    Open Access
    File
  • 153 Downloads (Pure)

    Nonlinear negative stiffness wing-tip spring device for gust loads alleviation

    Castrichini, A., Cooper, J. E., Wilson, T., Carrella, A. & Lemmens, Y., Jan 2017, 15th Dynamics Specialists Conference: AIAA SciTech Forum. American Institute of Aeronautics and Astronautics Inc. (AIAA), 27 p.

    Research output: Chapter in Book/Report/Conference proceedingConference Contribution (Conference Proceeding)

    Open Access
    File
  • 150 Downloads (Pure)

    Nonlinear Static Aeroelasticity of High Aspect Ratio Wing Aircraft by FEM and Multibody Methods

    Castellani, M., Cooper, J. E. & Lemmens, Y., Mar 2017, In : Journal of Aircraft. 54, 2, p. 548-560 13 p.

    Research output: Contribution to journalArticle (Academic Journal)

    Open Access
    File
  • 9 Citations (Scopus)
    316 Downloads (Pure)