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- W2018028596 abstract "Limit cycle oscillations in roll of advanced aircraft can result from three different fluid mechanical flow processes. The so-called slender wing rock is caused by asymmetric vortex shedding from highly swept wing leading edges. A completely different flow mechanism causes wing rock for aircraft with moderately swept leading edges. In this case, the causative mechanism is dynamic airfoil stall" @default.
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- W2018028596 date "1990-06-01" @default.
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- W2018028596 title "Various sources of wing rock" @default.
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- W2018028596 doi "https://doi.org/10.2514/3.25309" @default.
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