Environmental Engineering Reference
In-Depth Information
R
m
g
2
d
x
M
=
ò
0
R
ò
M
R
=
mr
g
d
x
0
R
ò
M
B
=
e
h
m
g
d
x
0
R
ò
M
g
=
m
g
d
x
0
R
ò
EI
z
(
g
)
2
d
x
K
B
=
0
R
ò
T
W
(x)(g )
2
d
x
K
W
=
0
R
I
hh
( g )
2
D
X
ò
K
q
=
I
hh
(
R
) g (
R
) g (
L
) -
0
r
(11-32)
T
c
(x)( g )
2
d
x
K
c
=
ò
0
R
ò
F
a
=
dA
z
g
d
x
0
R
ò
T
W
(x) =
mrd
x
x
RT
ò
T
c
(x) =
m
g
d
x
x
R
ò
T
g
(x) =
md
x)
x
After a trim solution has been found or after each revolution of a yaw-motion solution, the
flap displacement, slope, and velocity can be computed from the following equations:
(11-33a)
v
=
s
(
t
) g (x)
(11-33b)
v
=
s
(
t
) g (x)
v
=
s
(
t
) g (x)
(11-33c)
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