An experimental investigation of the flow through inclined circular tubes at a mach number of 4.0
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An experimental investigation of the flow through inclined circular tubes at a mach number of 4.0
P. L. Roe
URI:
https://reports.aerade.cranfield.ac.uk/handle/1826.2/897
Date:
1966
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Aeronautical Research Council Current Papers
[1393]
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