ESDU AERO A.06.01.00
Information on the use of Data Items on rolling moment derivatives of an aircraft.
Abstract:
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.Indexed under:
- Derivatives
- Rolling Moment
- Rolling Moment Due To Rolling (Lp or Clp)
- Rolling Moment Due To Sideslip (Lv or Cl β)
- Rolling Moment Due To Yawing (Lr or Clr)
Details:
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