ESDU AERO A.07.01.00 G
ESDU AERO A070100 G 1986-OCT-01 nformaton on the use of Data tems on yawng moment and sdeforce dervatves of an arcraft
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ESDU Aero A.07.01.00 gives brief details of the methods provided in the Series for the estimation of yawing moment and sideforce aerodynamic derivatives due to sideslip, rolling and yawing. The methods rely on estimating the contributions due to the various components of the aircraft separately and adding the part derivatives so obtained.