Problem 5.115
One of the wings of a Cessna 172 airplane is shown. The wing is supported by
a strut
BE
with ball-and-socket joints at
B
and
E
, and by bearings at
A
and
F
. The bearings are perfectly aligned and are supported by a straight shaft
which is fixed to the fuselage, and bearing
A
is a thrust bearing. Bearings
A
and
F
lie on the
x
axis, point
B
lies on the
y
axis, point
E
lies on the
´
axis,
and points
C
and
D
lie in the
xy
plane. The plane’s mass, including fuel,
passengers, and cargo, is
1000 kg
, and it flies so that it is in static equilibrium.
The strut
BE
has negligible mass and the wing
ABCDF
has
200 kg
mass
with center of gravity at point
B
. The force
Q
acts in the
x
direction and is
due to air drag. Remark: A two-dimensional model of this wing was treated
in Prob. 5.27 on p. 293.
(a)
Determine the resultant lift force
P
that this wing supports, assuming
this force is vertical and that only the wings provide lift for the plane.
(b)
If the drag force
Q
is
10
% of the lift force
P
, determine the force
supported by the strut BE and the reactions at bearings Aand F.