Research output

  1. System identification of the simulated in-flight loads

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

  2. Aeroelastic loads modeling for composite aircraft design support

    Research output: ThesisDissertation (TU Delft)Scientific

  3. Modified intertially coupled equqtions of motion for a flexible aircraft with coupled vibrations

    Research output: Contribution to journalArticleScientificpeer-review

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ID: 301338