dc.contributor.author |
M.J. Pratt |
en_US |
dc.date.accessioned |
2014-10-20T11:05:03Z |
|
dc.date.available |
2014-10-20T11:05:03Z |
|
dc.date.issued |
1967 |
en_US |
dc.identifier.other |
ARC/CP-1002 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/1015 |
|
dc.description.abstract |
The free piston compression shock tube provides a simple means of obtaining shock Mach numbers of the order of 30. This paper concerns the design and development at Cranfield of such a shock tube. The problems encountered in evolving a piston capable of withstanding heavy impacts at the completion of its stroke are outlined, and some preliminary shock tube performance data given. |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Current Papers |
en_US |
dc.title |
The development at Cranfield of a free piston compression shock tube |
en_US |