dc.contributor.author | G. H. Greenwood | en_US |
dc.date.accessioned | 2014-10-21T15:50:12Z | |
dc.date.available | 2014-10-21T15:50:12Z | |
dc.date.issued | 1968 | en_US |
dc.identifier.other | ARC/R&M-3625 | en_US |
dc.identifier.uri | https://reports.aerade.cranfield.ac.uk/handle/1826.2/2893 | |
dc.description.abstract | Pressure and heat-transfer measurements have been made on the lee surface of a delta wing at 14 degrees incidence in free flight over a Mach number range of 1.0 to 3.6 and at free-stream Reynolds numbers between 6 and 24 millions based on centreline chord. A comparison is made with the results from a previous free-flight model test to assess the effect on the lee surface pressure and heat transfer of a change in sweepback angle from 65.9 to 76 degrees. | en_US |
dc.relation.ispartofseries | Aeronautical Research Council Reports & Memoranda | en_US |
dc.title | Free-flight measurements of pressure and heat transfer on the lee surface of a delta wing at incidence (M = 1.0 to 3.6) | en_US |