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Calculated low-speed steady and time-dependent aerodynamic derivatives for some airfoils using a discrete vortex method
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Authors:
Riley, Donald R.
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Langley Research Center
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United States.
Year: 2015 Publisher: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center,
Year: 2015 Publisher: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center,
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Book
Piloted simulation study of an ILS approach of a twin-pusher business/commuter turboprop aircraft configuration
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Authors:
Riley, Donald R.
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Brandon, Jay M.
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Glaab, Louis J.
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Langley Research Center
Year: 1994 Publisher: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center,
Year: 1994 Publisher: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center,
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