Measurement of the Internal Performance of a Rectangular Air Intake having Variable Geometry Compression Surfaces at Mach Numbers from 1.7 to 2.5. Part 11 The Effect of Incidence

dc.contributor.author	C. S. Brown	en_US
dc.contributor.author	E. L. Goldsmith	en_US
dc.date.accessioned	2014-10-20T11:06:19Z
dc.date.available	2014-10-20T11:06:19Z
dc.date.issued	1973	en_US
dc.identifier.other	ARC/CP-1242	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/1255
dc.description.abstract	Measurements have been made of the internal performance of a rectangular intake having variable geometry compression surfaces. The measurements have been made within a range of Mach numbers from 1.7 to 2.46 and at angles of incidence up to 10°. The Reynolds number based on intake height was about 1.5 x 10	en_US
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	Measurement of the Internal Performance of a Rectangular Air Intake having Variable Geometry Compression Surfaces at Mach Numbers from 1.7 to 2.5. Part 11 The Effect of Incidence	en_US