dc.contributor.author |
D. C. Jenkins |
en_US |
dc.contributor.author |
J. D. Booker |
en_US |
dc.contributor.author |
J. W. Sweed |
en_US |
dc.date.accessioned |
2014-10-21T15:55:06Z |
|
dc.date.available |
2014-10-21T15:55:06Z |
|
dc.date.issued |
1958 |
en_US |
dc.identifier.other |
ARC/R&M-3203 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/3774 |
|
dc.description.abstract |
A description is given of apparatus developed at the Royal Aircraft Establishment for the study of the impact between a liquid drop and a surface moving at speeds up to 3,500 ft/sec. Some results obtained are briefly described and other possible uses for the apparatus discussed. |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Reports & Memoranda |
en_US |
dc.title |
An experimental method for the study of the impact between a liquid drop and a surface moving at high speed |
en_US |