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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?
shock wave
choke
expansion fan
stall
2)
How can lift be obtained at zero angle of attack?
leading edge nose radius
twist
camber
laminar flow
3)
How can flow be reattached at high angles of attack?
induce laminar boundary layer
increase viscosity
induce turbulent boundary layer
induce vorticity
4)
How can the Maximum Lift Coefficient be improved on an airfoil?
laminar boundary layer
sharp leading edge
smooth surface finish
camber
5)
The variation of Drag coefficient with angle of attack is expected to be
linear
exponential
logarithmic
quadratic
Cite this Simulator:
vlab.amrita.edu,. (2015). Wind Tunnel - Angle. Retrieved 21 January 2025, from vlab.amrita.edu/?sub=77&brch=297&sim=1684&cnt=3
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