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.
AERO A.6.01.00 J-2013由ESDU - Engineering Sciences Data Unit 发布于 2013-05-01,并于 2015-11-20 实施。
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