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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?
expansion fan
shock wave
stall
choke
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 turbulent boundary layer
increase viscosity
induce laminar boundary layer
induce vorticity
4)
How can the Maximum Lift Coefficient be improved on an airfoil?
sharp leading edge
laminar boundary layer
smooth surface finish
camber
5)
The variation of Drag coefficient with angle of attack is expected to be
linear
exponential
quadratic
logarithmic
Cite this Simulator:
vlab.amrita.edu,. (2015). Wind Tunnel - Angle. Retrieved 2 May 2024, from vlab.amrita.edu/?sub=77&brch=297&sim=1684&cnt=3
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