ESDU 82011:2013

$89.05

Estimation of side force and yawing moment derivatives due to sideslip for complete aircraft at subsonic speeds

Published By	Publication Date	Number of Pages
ESDU	2013-04-01	28

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Category: ESDU

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Description

ESDU 82011 illustrates the estimation of the sideforce and
yawing moment derivatives due to sideslip for complete aircraft at
subsonic speeds. It shows how to combine the ESDU methods for
predicting the contribution of the separate parts of the aircraft.
It covers cruise, landing and take-off configurations and is
applicable where there is a linear variation of lift coefficient
with angle of attack and of sideforce and yawing moment coefficient
with angle of sideslip. The computer program ESDUpac A0025,
associated with ESDU 00025, calculates the stability derivatives
treated in this Item.