Research output

  1. Multi-Fidelity Design of an Aeroelastically Tailored Composite Wing for Dynamic Wind-Tunnel Testing

    Research output: Chapter in Book/Report/Conference proceedingConference contributionScientificpeer-review

  2. Aeroelastic optimization of composite wings including fatigue loading requirements

    Research output: Contribution to journalArticleScientificpeer-review

  3. Preliminary aeroelastic design of composite wings subjected to critical gust loads

    Research output: Contribution to journalArticleScientificpeer-review

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ID: 214983