The influence of pressure ratio and divergence angle on the shock position in two dimensional, over-expanded, convergent-divergent nozzles
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The influence of pressure ratio and divergence angle on the shock position in two dimensional, over-expanded, convergent-divergent nozzles
P. F. Ashwood
;
G. W. Crosse
URI:
https://reports.aerade.cranfield.ac.uk/handle/1826.2/340
Date:
1957
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Aeronautical Research Council Current Papers
[1393]
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