A calculation method for the turbulent boundary layer on an infinite yawed wing in compressible, adiabatic flow
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A calculation method for the turbulent boundary layer on an infinite yawed wing in compressible, adiabatic flow
P. D. Smith
URI:
https://reports.aerade.cranfield.ac.uk/handle/1826.2/1281
Date:
1974
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Aeronautical Research Council Current Papers
[1393]
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