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

• Main Authors: C.M., Nur Syazwani, M. Nasir, Rizal E.
• Format: Article
• Language: English
• Published: Faculty of Mechanical Engineering Universiti Teknologi MARA (UiTM) 2017
• Subjects: TJ Mechanical engineering and machinery; Aeronautics. Aeronautical engineering
• Online Access: http://ir.uitm.edu.my/id/eprint/39122/1/39122.pdf; http://ir.uitm.edu.my/id/eprint/39122/

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...