INFINITE WING
Model of infinite
wingspan in the test section of the wind tunnel is through and through. The flow about
infinite wing is 2 dimensional i.e. in X & Y direction, as it is ±∞ in the Z direction. Lift, Drag, Moment coefficient for the infinite wing
is represented as CL, CD, CM, (capital letters).
FINITE WING
The finite wing is defined wingspan (distance between two wingtips, denoted as b)
Which means
the flow about finite wing is 3 dimensional i.e. the flow over the wing is in X & Y & Z direction. Lift, Drag, Moment coefficient are represented as Cl, Cd, Cm, (small letters).
HIGH WING
The wing is placed on the top of the fuselage i.e. the centre of gravity (Cg). It is a negative distance w.r.t. aerodynamic centre (ag) in the Z direction as shown in the figure. Aerodynamic centre is a point where the sum of all aerodynamic forces is equal to 0. This is called a high wing. It is more stable as compared to the mid and low wing.
MID WING
The wing is placed where the centre of gravity and aerodynamic centre have 0 distance in the Z direction. It is less stable than a high wing and more stable than the low wing
LOW WING
The wing is placed on the bottom of the fuselage i.e. centre of gravity is a positive distance w.r.t. aerodynamic centre in Z direction it is called a low wing. It is very less stable as compared to the mid and high wing
TYPES OF WING ON THE BASES OF ASPECT RATIO
Where Cd,i = induced drag
CL=
lift coefficient
AR=
aspect ratio
As from the above equation, we can intuition that higher the
aspect ratio less the induced drag
Elliptic wing
elliptic wing: this type of wing, it has a high
aspect ratio. We don’t use this type of wing because it is expensive to
manufacture
Rectangular wing
Rectangular wing: in this type of wing it has a low aspect ratio i.e. the lift distribution far from optimum.
Tapered wing
Tapered wing: in this type of wing the aspect
ratio is lower than an elliptic wing and higher than a rectangular wing. Commercial aircraft have tapered wing because
it is easy to manufacture
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