Evolution of disturbances in a laminarized supersonic boundary layer on a swept wing.
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- Journal of Applied Mechanics & Technical Physics, 2008, v. 49, n. 2, p. 188, doi. 10.1007/s10808-008-0027-1
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Works matching DE "SWEPT-back wings (Airplanes)"
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Investigation potential flow about swept back wing using panel method.
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- International Journal of Energy & Environment, 2016, v. 7, n. 4, p. 317
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- Article