ESDU AERO A.06.01.00 I
ESDU AERO A060100 1986-OCT-01 nformaton on the use of Data tems on rollng moment dervatves of an arcraft
Cart
(empty)
ESDU Aero A.06.01.00 gives brief details of the methods provided in the Series for the estimation of rolling moment 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.