Effects of Angle of Attack, Aspect Ratio, and Leading-Edge Curvature on Supersonic Fin Performance

Effects of Angle of Attack, Aspect Ratio, and Leading-Edge Curvature on Supersonic Fin Performance

The aerodynamic optimization of fin-stabilized rockets operating under supersonic conditions remains a critical challenge in aerospace enginnering. Current studies often fail to capture the combined effects of multiple geometric parameters on aerodynamic performance. This research employs a full-fac...

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Bibliographic Details
Main Authors: M. Hasbi Ash Shiddieqy, Andoko Andoko
Format: Article
Language:English
Published: Lembaga Penelitian dan Pengabdian Masyarakat (LPPM), Universitas Andalas 2025-07-01
Series:Andalasian International Journal of Applied Science, Engineering, and Technology
Online Access:https://aijaset.lppm.unand.ac.id/index.php/aijaset/article/view/243
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