Analysis of flow characteristics around sharp, blunt, and bulb-shaped missile nose geometries

The current study investigates the aerodynamic characteristics of three distinct missile nose cone geometries: sharp, blunt, and bulb-shaped under supersonic conditions at Mach numbers 2.4, 2.8, 3.2, and 3.6. The primary objective is to analyze key parameters, such as lift and drag coefficients, an...

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Bibliographic Details

Main Authors:	Shetty, Shamitha, Nagarkar, Kavana, Khan, Sher Afghan, Aabid, Abdul, Baig, Muneer
Format:	Article
Language:	en en
Published:	Elsevier Ltd. 2025
Subjects:	TL780 Rockets
Online Access:	http://irep.iium.edu.my/121818/7/121818_%20Analysis%20of%20flow%20characteristics.pdf http://irep.iium.edu.my/121818/13/121818_Analysis%20of%20flow%20characteristics_Scopus.pdf http://irep.iium.edu.my/121818/ https://www.sciencedirect.com/science/article/pii/S266620272500268X https://doi.org/10.1016/j.ijft.2025.101321
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