Free-flight measurements of pressure and heat transfer on the lee surface of a delta wing at incidence (M = 1.0 to 3.6)

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