Research output

  1. Preliminary Sizing Method for Hybrid-Electric Distributed-Propulsion Aircraft

    Research output: Contribution to journalArticleScientificpeer-review

  2. A preliminary sizing method for hybrid-electric aircraft including aero-propulsive interaction effects

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

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Activities

  1. Flying V

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

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ID: 16882473