Research output

  1. Experimental evaluation of a morphing leading edge concept

    Research output: Contribution to journalArticleScientificpeer-review

  2. Flexible Aircraft Gust Load Alleviation with Incremental Nonlinear Dynamic Inversion

    Research output: Contribution to journalArticleScientificpeer-review

  3. Transonic flight and movable load modelling for wing-box preliminary sizing

    Research output: Chapter in Book/Report/Conference proceedingConference contributionScientific

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Activities

  1. State-of-the-art challenges of morphing wing conceptual design

    Activity: Talk or presentationTalk or presentation at a workshop, seminar, course or other meeting

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ID: 220521