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

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...

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Bibliographic Details

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