The pressure calibration of the R.A.E. 6 inch diameter shock tube with a view to its use as the driver of a cold high-density hypersonic tunnel
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The pressure calibration of the R.A.E. 6 inch diameter shock tube with a view to its use as the driver of a cold high-density hypersonic tunnel
S. G. Cox
;
R. J. Pallant
;
J. M. Shaw
URI:
https://reports.aerade.cranfield.ac.uk/handle/1826.2/711
Date:
1963
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Aeronautical Research Council Current Papers
[1393]
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