Authors: Saraniyan M, Assistant professor Gowtham G
Abstract: The Unmanned Combat Aerial Vehicle (UCAV) Ghatak represents a pivotal advancement in stealth and autonomous aerial warfare technology. This project focuses on a comprehensive aerodynamic analysis of the Ghatak UCAV using Computational Fluid Dynamics (CFD) tools. By simulating realistic flight conditions, this study evaluates the aerodynamic performance parameters such as lift, drag, pressure distribution, and flow behavior across the stealth-designed airframe. The analysis takes into account various angles of attack and flight regimes to understand the aircraft’s stability and efficiency. The objective is to optimize the aerodynamic characteristics of Ghatak to ensure superior performance, maneuverability, and reduced radar signature. The insights gained from this CFD-based investigation will contribute to enhancing the combat readiness and operational effectiveness of next-generation UCAVs.
