ESDU AERO A.07.01.00
Information on the use of Data Items on yawing moment and sideforce derivatives of an aircraft
Abstract:
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.Indexed under:
- Derivatives
- Sideforce
- Yawing
- Yawing Moment Due To Rolling (Np or Cnp)
- Yawing Moment Due To Sideslip (Nv or Cnβ)
- Yawing Moment Due To Yawing (Nr or Cnr)
Details:
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