Problem 5.27
The front view of one of the wings of a Cessna 172 airplane is shown. The
wing is supported by a pin-connected strut
BE
and by a connection at
A
that
may be idealized as a pin. 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
ABCD
has
200 kg
mass with center of gravity
at point
B
. Model the wing as a two-dimensional structure where all forces lie
in the same plane.
(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) Determine the forces supported by the strut BE and the pin at A.
Solution
Part (a)
The FBD for the airplane is shown, where the weight is
WD1000 kg 9:81 m
s2D9810 N:(1)
The equilibrium equation is
XFyD0W2P WD0)PD4905 N. (2)
Part (b)
The FBD for the wing is shown at the right, where the
weight of the wing is
WwD200 kg 9:81 m
s2D1962 N. (3)
XMAD0WP .2:6 m/Ww.2 m/TBE
1:4
p5:96.2 m/D0)TBE D7698 N, (4)
XFxD0WAxTBE
2
p5:96 D0)AxD6306 N;(5)
XFyD0WAyTBE
1:4
p5:96 WwCPD0)AyD1472 N:(6)
May 11, 2012
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