Tests of Humidity Effects on Flow in a Wind Tunnel at Mach Numbers between 2.48 and 4
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Tests of Humidity Effects on Flow in a Wind Tunnel at Mach Numbers between 2.48 and 4
R. J. Monaghan M.A.
URI:
https://reports.aerade.cranfield.ac.uk/handle/1826.2/260
Date:
1956
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Aeronautical Research Council Current Papers
[1393]
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