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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
stall
choke
shock wave
2)
How can lift be obtained at zero angle of attack?
laminar flow
camber
twist
leading edge nose radius
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?
smooth surface finish
laminar boundary layer
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 29 March 2024, from vlab.amrita.edu/index.php?sub=77&brch=297&sim=1684&cnt=3
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