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Boundary Layer Thickness in Wind Tunnel by liristhika711 is a document available to read on EtoBox.
This document details an experiment conducted to estimate the boundary layer thickness in a low-speed wind tunnel, focusing on velocity distribution and the behavior of the boundary layer. The study utilizes a pitot-static tube for pressure measurements and analyzes laminar and turbulent flow characteristics to enhance aerodynamic performance understanding. Key findings include the calculation of Reynolds number, boundary layer thickness, displacement thickness, and momentum thickness based on experimental
- Author
- liristhika711
- Language
- EN