The Effects of Tail-Tilt on the Yaw Stability of Baseline-V Blended Wing Body Aircraft / Nur Syazwani C.M and Rizal E.M. Nasir

• 主要な著者: C.M., Nur Syazwani (著者), M. Nasir, Rizal E. (著者)
• フォーマット: 図書
• 出版事項: Faculty of Mechanical Engineering Universiti Teknologi MARA (UiTM), 2017.
• 主題: Article; PeerReviewed
• オンライン･アクセス: Link Metadata

This paper presents a study on the effects of tilting the tail on yaw stability performance of Baseline-V blended wing body (BWB) aircraft. The study on BWB aircraft began in UiTM in 2005 and a few designs of BWB aircraft have been studied and published. Recent progress on BWB study in UiTM indicate...