dc.contributor.author |
H.E. Gamble |
en_US |
dc.date.accessioned |
2014-10-20T11:00:09Z |
|
dc.date.available |
2014-10-20T11:00:09Z |
|
dc.date.issued |
1951 |
en_US |
dc.identifier.other |
ARC/CP-103 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/116 |
|
dc.description.abstract |
An untapered, sweptback wing of aspect ratio 4, sweepback 25 degrees and section 12% thick (R.A.E. 104 with 1% camber, a = 0.6) was tested in the R.A.E. Hqh Speed Tunnel. The pressure distribution was measured at the mid-semispan section at various Mach numbers up to 0.88 at Reynolds numbers of 0.8, 1.8 and 3.5 x 10 to the power 6. |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Current Papers |
en_US |
dc.title |
Some effects of Reynolds number on a cambered wing at high subsonic Mach numbers |
en_US |