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Vortex development for a 65 degree swept back delta wing with varying thickness and maximum thickness location (2020)
Thesis
Stucke, J. Vortex development for a 65 degree swept back delta wing with varying thickness and maximum thickness location. (Thesis). University of the West of England. Retrieved from https://uwe-repository....ribe.com/output/6012701

Low signature, unmanned combat aerial vehicles (UCAV) are foreseen to play an important role in future military missions. Most UCAV concepts feature some sort of delta or lambda type of wing with high or moderately swept leading edge, where the fusel... Read More about Vortex development for a 65 degree swept back delta wing with varying thickness and maximum thickness location.