Research output

  1. Ground Testing of the FLEXOP Demonstrator Aircraft

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

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

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

  3. Results of an Aeroelastically Tailored Wing on the FLEXOP Demonstrator Aircraft

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

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ID: 218033