398 Alex Goodman 
Table 2 
Reduction Equations for Rotary and Acceleration Derivatives* 
Vertical Plane 
_ OZ "Din + (22dinl O02, ')in + Za" dinl 
wae ae a 
aes ol(Z,'), = (Z,")i nl x el(2, din > (Z,')i 41 
t ow, 4 ow, 
° 
UZ" dour + aJoued — UZ "dour + Fr'Jourl 
2q,' ; 2q,' 
x Ol(Z 2" dour ry (2; Douel CZ a" dour ~ (21 Jour! 
iv eM ae - 
Hees 
°q,’ 4 aq,’ 
MCE Di CAS OZ int ain 
2g,’ 0g," 7 
x (2Z,')in = i Jinl es 2002 4"Jin ~ 1'Dinl 
4 oq," w? 4 0q,' w? 
Horizontal Plane 
Safar Bo 
atC¥ "din + Pa ial Din * Pa"dinl 
r ov,’ ov,” 
' 
Me 
x CK, 7 sind ie sin 7 M1 ind 
a ov,’ q ov,’ 
= Os Dour ¥ a out! i OLCK dour y CADE! 
‘ , 
or, or, 
OLY a" Jout ot CY ourd ah OK a Dour i Cia Dane 
or,’ 4 ae” 
Cle Suet vy Y,')inl Cle Fae Sh (Ye dinl 
“ or,’ or,' 
xe OlLOXa ite Olan inl ri MOG Oy SOO) ioe 
a [o Waco) mua eat Stop or,’ 
LXKD CK" )in 
3, Ww," 
° 
OK") out + O(K') out 
2 chen’ or, 
2 ie OK'd in 
oe” or.’ 
o 
= AK dour S OK") out 
ep,’ op,’ 
* mys (Mod m Ny) m> and (K,),, determined from standstill tests 
