dc.contributor.author |
W. E. Gray |
en_US |
dc.date.accessioned |
2014-10-20T11:05:36Z |
|
dc.date.available |
2014-10-20T11:05:36Z |
|
dc.date.issued |
1970 |
en_US |
dc.identifier.other |
ARC/CP-1090 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/1103 |
|
dc.description.abstract |
Flow visualization techniques, which have been successfully used in flight tests, are described. One indicates boundary-layer transition on a wing with a "china clay" coating, that is wetted at high altitude with a liquid of suitable volatility emitted by another aircraft; the result is photographed at altitude. The second shows the shock-wave position by the differential rippling of a viscous oil coating on the wing; it also reveals laminar flow areas by unrippled oil, at the same time. It relies on direct sunlight but is not over-sensitive to the direction of this, within quite wide limits. Comparative shock-wave results are given using an earlier direct sun-shadowgraph method which requires precise sun alignment and has been little used. |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Current Papers |
en_US |
dc.title |
A brief account of some unrecorded techniques for flow visualization in flight for locating (a) boundary layer transition at altitude, (b) shock-wave position |
en_US |