Design and operating features of the N.P.L. 6 in. shock tunnel
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Design and operating features of the N.P.L. 6 in. shock tunnel
L. Pennelegion
;
R. F. Cash
;
D. F. Bedder
URI:
https://reports.aerade.cranfield.ac.uk/handle/1826.2/4030
Date:
1965
Abstract:
Engineering aspects of the shock tunnel facility are described. Details of gas services and routine instrumentation are given. The performance envelope of the tunnel is discussed and routine measurements presented.
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Aeronautical Research Council Reports & Memoranda
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