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Higher Hydrodynamic Analysis on Marlin Glider wing Torpedo’s
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Black Marlin is a fish-adopted design that will be integrated to the fastest and will be deployed at high altitudes from the fixed glider wing. The Black Marlin torpedo will be controlled by a GPS/INS-based navigation system. This research will help with Three-dimensional movement simulation and dynamic modelling motion of an underwater Black Marlin glider wing torpedo shape. The case of computational fluid dynamics (CFD) analysis was performed using the hydrodynamic parameter generated from tests such as the moment of lift, drag and erection at different angles of attack, where the varying Reynolds numbers around 106 were studied and the static flow velocity was 10.5 m/s and the body angle ranged from - 100 to 100 in steps of 5° for National Advisory Committee for Aeronautics (NACA) glider wing design configurations are used to assess torpedo performance across the entire operational area. The principal purpose of this project is to compare results obtained for different models like Circular, Elliptical and Black Marlin glider wing Torpedo using analysis software. We can deduce from the results that the Black marlin glider wing Torpedo delivers a lot of lift, drag, pitching moment, and velocity forces. CATIA Software was utilized to design Generative Shape Design and Assembly Design. The analysis is done using the ANSYS Fluent software.
Title: Higher Hydrodynamic Analysis on Marlin Glider wing Torpedo’s
Description:
Black Marlin is a fish-adopted design that will be integrated to the fastest and will be deployed at high altitudes from the fixed glider wing.
The Black Marlin torpedo will be controlled by a GPS/INS-based navigation system.
This research will help with Three-dimensional movement simulation and dynamic modelling motion of an underwater Black Marlin glider wing torpedo shape.
The case of computational fluid dynamics (CFD) analysis was performed using the hydrodynamic parameter generated from tests such as the moment of lift, drag and erection at different angles of attack, where the varying Reynolds numbers around 106 were studied and the static flow velocity was 10.
5 m/s and the body angle ranged from - 100 to 100 in steps of 5° for National Advisory Committee for Aeronautics (NACA) glider wing design configurations are used to assess torpedo performance across the entire operational area.
The principal purpose of this project is to compare results obtained for different models like Circular, Elliptical and Black Marlin glider wing Torpedo using analysis software.
We can deduce from the results that the Black marlin glider wing Torpedo delivers a lot of lift, drag, pitching moment, and velocity forces.
CATIA Software was utilized to design Generative Shape Design and Assembly Design.
The analysis is done using the ANSYS Fluent software.
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