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Coupled Flight Mechanics based on Reduced Order Models for use in Tiltrotor Stability Analysis

Research output: Chapter in Book/Report/Conference proceedingConference Contribution (Conference Proceeding)

5 Citations (Scopus)
Original languageEnglish
Title of host publicationAIAA Aviation Forum 2019
PublisherAmerican Institute of Aeronautics and Astronautics Inc. (AIAA)
DOIs
Publication statusPublished - 15 Jun 2019

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