Can anyone please help me in this problem of reducing "wind shear effect on an aircraft wing"? My friend just initiated this project entitled "transport modelling to reduce wind shear effect on an aircraft wing". He even don't know how to approach this.
Any literature? reference? Anything related to the same?
Thanks a ton in advance.
This has to do with the proper design on the wings of aircraft which prevents abrupt separation of boundary layer attached to the wings. Often NACA aerofoil is used to simulate the wind shear effect. At different wind velocities, drag and lift coefficients are evaluated and geometry is optimized for minimum drag coefficient. This is a standard problem in CFD and many references are available.
This has to do with the proper design on the wings of aircraft which prevents abrupt separation of boundary layer attached to the wings. Often NACA aerofoil is used to simulate the wind shear effect. At different wind velocities, drag and lift coefficients are evaluated and geometry is optimized for minimum drag coefficient. This is a standard problem in CFD and many references are available.
Thank you Mr. Mitra,
Can you please attach those references or links. Anything will be fine.
Regards
Check out this one.
http://www.academicjournals.org/article/article1379753908_Eleni%20et%20al.pdf
And just google with NACA aerofoil + CFD and plenty of references will pop up.
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