Relaxed Static Stability Performance Assessment on Conventional and Unconventional Aircraft Configurations

Master Thesis (2015)
Author(s)

Q.J.M. Jansen

Contributor(s)

R. Vos – Mentor

Copyright
© 2015 Jansen, Q.J.M.
More Info
expand_more
Publication Year
2015
Copyright
© 2015 Jansen, Q.J.M.
Reuse Rights

Other than for strictly personal use, it is not permitted to download, forward or distribute the text or part of it, without the consent of the author(s) and/or copyright holder(s), unless the work is under an open content license such as Creative Commons.

Abstract

This thesis report researches the influence of a reduced stability margin on the aircraft performance of conventional and unconventional aircraft configurations. Unconventional configurations are defined as canard and three-surface aircraft.

Files

License info not available