An effect of sweep angle on roll damping derivative for a Delta wing with curved leading edges in unsteady flow

An effect of sweep angle on roll damping derivative for a Delta wing with curved leading edges in unsteady flow

This paper presents the results of an analytical study to account the effect of the sweep angle of a delta wing whose leading edges are curved on roll damping derivative at various angles of attack and the amplitude of the full sine waves. In the present theory, the effect of Leeward surface has b...

Full description

Bibliographic Details
Main Authors: Monis, Renita Sharon, Crasta, Asha, Khan, Sher Afghan
Format: Article
Language:English
English
Published: Transstellar Journal Publications and Research 2019
Subjects:
TL787 Astronautics
Online Access:http://irep.iium.edu.my/70995/
http://irep.iium.edu.my/70995/1/70995_An%20effect%20of%20sweep%20angle%20on%20roll%20damping.pdf
http://irep.iium.edu.my/70995/2/70995_An%20effect%20of%20sweep%20angle%20on%20roll%20damping_Scopus.pdf

Similar Items

Similar Items