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Mechanical Engineering
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Wind energy Labs
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Wind Tunnel - Angle
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Wind Tunnel - Angle
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Wind Tunnel Fundamentals
Theory
Procedure
Self Evaluation
RT
Assignment
Reference
Feedback
Data Set
1)
Why can't the lift-curve slope be maintained at high angles of attack?
choke
shock wave
expansion fan
stall
2)
How can lift be obtained at zero angle of attack?
twist
leading edge nose radius
laminar flow
camber
3)
How can flow be reattached at high angles of attack?
induce vorticity
induce laminar boundary layer
increase viscosity
induce turbulent boundary layer
4)
How can the Maximum Lift Coefficient be improved on an airfoil?
laminar boundary layer
smooth surface finish
sharp leading edge
camber
5)
The variation of Drag coefficient with angle of attack is expected to be
quadratic
linear
logarithmic
exponential
Cite this Simulator:
vlab.amrita.edu,. (2015). Wind Tunnel - Angle. Retrieved 17 January 2026, from vlab.amrita.edu/?sub=77&brch=297&sim=1684&cnt=3
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