Preliminary measurements in a shock tunnel of shock angle and undersurface pressure related to a nonweiler wing
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Preliminary measurements in a shock tunnel of shock angle and undersurface pressure related to a nonweiler wing
L. Pennelegion
;
R. F. Cash
URI:
https://reports.aerade.cranfield.ac.uk/handle/1826.2/697
Date:
1963
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Aeronautical Research Council Current Papers
[1393]
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