39
0RGHO%DVLF6HWWLQJ3URFHGXUH!
IRUHDFKFRQGLWLRQ$WLQLWLDOVHWWLQ
 system and set this curve to 
mb at a 
constant speed.
ŏ3
 stall turn, loop, and roll
ght 
ahead when heading into the wind
This function is set so that the fuselage is facing
strai
ht line auto rotation. The 
pitch of the tail rotor becomes nearly 
7KURWWOHKROGVHWWLQJ
,IWKURWWOHKROGLVQHFHVVDU
SOHDVHUHIHUWRWKH7+5+2/'
IXQFW
RQS
7KURWWOHFXWVHWW
KURWWOHFXWSURYLGHVDQHDV
e
WRDYRLGDFFLGHQWDOGHDGVWLFNV7KHVZLWFK¶V
:LWKWKURWWOHVWLFNDWLGOHDGMXVWWKHFXWSRVLWLRQXQWLOWKH
HQJLQHFRQVLVWHQWO\VKXWVRIIEXWWKURWWOHOLQNDJHLVQRW
QGHOHYDWRU)RUZDUG$IW&
'5IXQFWLRQLVXVHGWRDG
HUDWLRQFXUYHRIDLOHURQHOHYDWRUDQGUXGGHUIRU
KLVLVQRUPDOO\XVHGDIWHU(QG3RLQWKDVGH¿QHG
W
H
PRGHODQGFDQEHVHWIRUHDFKFRQGLWLRQ
ŏ 1
3LWFKWR58'PL[LQJVHWWLQJ
Note: When usin
eaction torque is corrected by the 
RXZDQWWRVXSSUHVV
WKHWRUTXHJHQHUDWHGE\WKHFKDQJHVLQWKHSLWFK
an
XVWLWVRWKDWWKHQRVHGRHVQRWVZLQ
LQWKH
UXGGHUGLUHFWLRQ+RZHYHUZKHQXVLQJDKHDGLQJ
.
$FWLYDWHWKH3LWFKWRUXGGHU3LW!58'PL[LQJ
IXQFW