![Case setup for (a) unswept wing and (b) swept wing. (c) cross-sectional... | Download Scientific Diagram Case setup for (a) unswept wing and (b) swept wing. (c) cross-sectional... | Download Scientific Diagram](https://www.researchgate.net/publication/346372605/figure/fig1/AS:962174390386689@1606411659209/Case-setup-for-a-unswept-wing-and-b-swept-wing-c-cross-sectional-mesh-at-locations_Q320.jpg)
Case setup for (a) unswept wing and (b) swept wing. (c) cross-sectional... | Download Scientific Diagram
Effect of nose shape and trailing-edge bluntness on the aerodynamic characteristics of an unswept wing of aspect ratio 3.1, taper ratio 0.4, and 3-percent thickness - UNT Digital Library
Low-speed lateral-control characteristics of an unswept wing with hexagonal airfoil sections and aspect ratio 2.5 equipped with spoilers and with sharp- and thickened-trailing-edge flap-type ailerons at a Reynolds number of 7.6 x
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