Some measurements of shock-wave attenuation in channels of various cross-sections

dc.contributor.author	L. Bernstein	en_US
dc.date.accessioned	2014-10-21T15:55:52Z
dc.date.available	2014-10-21T15:55:52Z
dc.date.issued	1961	en_US
dc.identifier.other	ARC/R&M-3321	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3901
dc.description.abstract	Apparatus is described for the measurement of shock attenuation in channels of several configurations. A circular-bore channel, a square-bore channel and converging and diverging channels have been investigated. Measurements of hot-flow duration and wall pressure variations in the shock tube have also been made. It is concluded that convergence of the shock-tube channel provides an attractive method of alleviating attenuation, particularly since the hot-flow durations are not significantly altered by a slow convergence.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	Some measurements of shock-wave attenuation in channels of various cross-sections	en_US