A two-dimensional analysis on the flight of FL FN an airfoil is shown in the figure. The airfoil shape is traveling at a certain velocity and meets the incoming airflow at an angle of attack a. As shown, the forces affecting -FD the flight of the airfoil is the drag force a FA (FD), lift force (F) and the two other variable forces (Fn and Fa) acting normal and axial on the airfoil. The lift force (FL) on the airfoil is a function of its length L, velocity V, diameter D, angle of attack a, density p, viscosity µ, and speed of sound c of the air (i.e. F. = f(L, V, D, a, p, µ, c). Use dimensional analysis to show that the lift coefficient Cis a function of a set of dimensionless parameters. Also, is air temperature T, a significant variable in the function of the lift force? Use p,V,D and Ta as repeating variables.

Elements Of Electromagnetics
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Author:Sadiku, Matthew N. O.
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A two-dimensional analysis on the flight of
FN
FL
R
an airfoil is shown in the figure. The airfoil
shape is traveling at a certain velocity and
meets the incoming airflow at an angle of
attack a. As shown, the forces affecting
FD
the flight of the airfoil is the drag force
a
FA
(FD), lift force (F) and the two other
Voo
variable forces (FN and Fa) acting normal
and axial on the airfoil. The lift force (FL)
on the airfoil is a function of its length L, velocity V, diameter D, angle of attack a, density p,
viscosity µ, and speed of sound c of the air (i.e. FL = f(L, V, D, a, p, µ, c). Use dimensional
analysis to show that the lift coefficient C,is a function of a set of dimensionless parameters.
Also, is air temperature T, a significant variable in the function of the lift force? Use
p,V,D and Ta as repeating variables.
Transcribed Image Text:A two-dimensional analysis on the flight of FN FL R an airfoil is shown in the figure. The airfoil shape is traveling at a certain velocity and meets the incoming airflow at an angle of attack a. As shown, the forces affecting FD the flight of the airfoil is the drag force a FA (FD), lift force (F) and the two other Voo variable forces (FN and Fa) acting normal and axial on the airfoil. The lift force (FL) on the airfoil is a function of its length L, velocity V, diameter D, angle of attack a, density p, viscosity µ, and speed of sound c of the air (i.e. FL = f(L, V, D, a, p, µ, c). Use dimensional analysis to show that the lift coefficient C,is a function of a set of dimensionless parameters. Also, is air temperature T, a significant variable in the function of the lift force? Use p,V,D and Ta as repeating variables.
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