Difference between infinite and finite wings and the vortex caused by the finite wing is explained. The origin of downwash velocity is outlined. The change in the angle of attack seen by the finite wing and the effect of the induced angle of attack on the lift and drag coefficients are pointed out. The concept of induced drag is discussed.
#aerospaceengineering #gateaerospaceengineering
#aerodynamics
#fluidmechanics
Continue this lesson in the app
Install CourseHive on Android or iOS to keep learning while you move.
