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.
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
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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