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

• 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/70995/1/70995_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; http://irep.iium.edu.my/70995/; http://www.tjprc.org/publishpapers/2-67-1551420484-35IJMPERDAPR201935.pdf

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...