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...
Saved in:
| Main Authors: | , |
|---|---|
| Format: | Book |
| Published: |
Faculty of Mechanical Engineering Universiti Teknologi MARA (UiTM),
2017.
|
| Subjects: | |
| Online Access: | Link Metadata |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Internet
Link Metadata3rd Floor Main Library
| Call Number: |
A1234.567 |
|---|---|
| Copy 1 | Available |