dc.contributor.author |
A. S. Batson |
en_US |
dc.contributor.author |
J. H. Preston |
en_US |
dc.contributor.author |
J. H. Warsap |
en_US |
dc.date.accessioned |
2014-10-21T15:52:23Z |
|
dc.date.available |
2014-10-21T15:52:23Z |
|
dc.date.issued |
1943 |
en_US |
dc.identifier.other |
ARC/R&M-2698 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/3243 |
|
dc.description.abstract |
To add to the available data regarding lift and hinge moment on a control, and to test further the ideas developed in R. & M. 20O8, with especial reference to the effect of curvature of control surface. Measurement of lift and hinge moment on a two-dimensional aerofoil (section NACA 0015, chord 18 in.) fitted with a 40 per cent control (radius-nose). |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Reports & Memoranda |
en_US |
dc.title |
Experiments giving hinge moment and lift on a NACA 0015 aerofoil fitted with a 40 per cent control, with especial reference to effect of curvature of control surface |
en_US |