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- W4322748995 abstract "The wing area with a triangular planar shape is called delta wings. The supersonic flow is, in many respects, completely different from the subsonic flow. These differences affect the design philosophy of supersonic and subsonic aircraft. This research addresses subsonic flow and design on delta wings. CFD is being used to improve the delta wing’s efficiency in this project. An experiment necessitates the use of a design model, which is more time consuming and expensive than using CFD methods for the same purpose. A computational fluid dynamics model underpins the whole investigation. At different angles of attack of 0, 5, 10, 15, 20, the flow over a NACA0012 aerofoil is analysed in two dimensions. This analysis is performed by considering various parameters like temperature, pressure, and velocity using computational fluid dynamics using Software ANSYS2016." @default.
- W4322748995 created "2023-03-03" @default.
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- W4322748995 date "2023-01-01" @default.
- W4322748995 modified "2023-10-16" @default.
- W4322748995 title "Computational Fluid Dynamics Analysis of Delta Wing" @default.
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- W4322748995 doi "https://doi.org/10.1007/978-981-19-7971-2_66" @default.
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