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Gurney Flaps on Swept Wing Analysis by kevin9833252835 is a document available to read on EtoBox.

This project report summarizes experimental analysis of forward swept and swept back wings with Gurney flaps. A wing model with a span of 900mm and aspect ratio of 6 was designed and fabricated. The model was tested in a wind tunnel to analyze the effects of Gurney flaps on forward and backward swept wings. Pressure measurements from pressure ports on the wing surface along with tuft flow and smoke flow visualizations were used to generate data. MATLAB programs were used to plot lift coefficients and CP vs

Author

kevin9833252835

Language

EN