dc.contributor.author |
G. H. Greenwood |
en_US |
dc.date.accessioned |
2014-10-21T15:50:37Z |
|
dc.date.available |
2014-10-21T15:50:37Z |
|
dc.date.issued |
1970 |
en_US |
dc.identifier.other |
ARC/R&M-3679 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/2952 |
|
dc.description.abstract |
Pressure and heat-transfer measurements have been made in free flight on a caret wing with blunt leading edges and nose, at speeds below and above the design Mach number of 2.47. Comparison with data from a corresponding caret wing but with sharp leading edges indicates that the effect of blunting is confined to a region about 2 to 3 leading-edge diameters from the leading edge. At M∞ > 1.5 the data for the blunt leading edges and for the plane lifting surfaces were for the most part predicted with reasonable accuracy using easily-applied existing theory. A considerable reduction in heating rate was found in the wing junction. |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Reports & Memoranda |
en_US |
dc.title |
Free-flight measurements of pressure and heat transfer on a blunt leading-edge caret wing at design and off-design Mach numbers (M infinity = 0.9 to 3.36) |
en_US |