Method for calculating the rolling and yawing moments due to rolling for unswept wings with or without flaps or ailerons by use of nonlinear section lift data, by Albert P. Martina et al.

Title:	Method for calculating the rolling and yawing moments due to rolling for unswept wings with or without flaps or ailerons by use of nonlinear section lift data
Author:	Martina, Albert P.
Author:	United States. National Advisory Committee for Aeronautics
Note:	National Advisory Committee for Aeronautics, 1953

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Subject:	Aerofoils
Subject:	Airplanes -- Wings
Subject:	Lift (Aerodynamics)
Subject:	Mathematical analysis
Subject:	Rolling (Aerodynamics)
Subject:	Yawing (Aerodynamics)
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