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

Show simple item record

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


Files in this item

This item appears in the following Collection(s)

Show simple item record

Search AERADE


Browse

My Account