dc.contributor.author |
F. Cheers |
en_US |
dc.contributor.author |
W. G. Raymer |
en_US |
dc.contributor.author |
Ola Douglas |
en_US |
dc.date.accessioned |
2014-10-21T15:53:20Z |
|
dc.date.available |
2014-10-21T15:53:20Z |
|
dc.date.issued |
1947 |
en_US |
dc.identifier.other |
ARC/R&M-2355 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/3433 |
|
dc.description.abstract |
A series of tests on an 8.6 per cent thick nose-suction aerofoil designed by Lighthill has been made in the 4 ft No. 2 Wind Tunnel at the National Physical Laboratory at Reynolds numbers of 0.385 and 0.577 x 10(to the power of 6). The results show that the wing stalls at alpha ~= 3 deg (Cl = 1.12) without suction, the lift coefficient at the stall increasing approximately linearly with suction quantity and reaching 1.93 at Cq = 0.019 and 23 deg incidence. |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Reports & Memoranda |
en_US |
dc.title |
Tests on a 'lighthill' nose-suction aerofoil in the N.P.L. 4-ft. no. 2 wind tunnel |
en_US |