Research output

  1. The effects of a full-aircraft aerodynamic model on the design of a tailored composite wing

    Research output: Contribution to journalArticleScientificpeer-review

  2. The Effects of Aeroelastic Tailoring on Flight Dynamic Stability

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

View all (2) »

ID: 180051