An experimental investigation of the pressure distributions on five bodies of revolution at Mach numbers of 2.45 and 3.19

Marson, G. B.; Socha, W.; Keates, R. E.

dc.contributor.author	Marson, G. B.
dc.contributor.author	Socha, W.
dc.contributor.author	Keates, R. E.
dc.date.accessioned	2012-09-11T15:40:47Z
dc.date.available	2012-09-11T15:40:47Z
dc.date.issued	1954-04
dc.identifier.uri	http://dspace.lib.cranfield.ac.uk/handle/1826/7565
dc.description.abstract	Measurements have been made in the College of Aeronautics 2½ x2½ intermittent high speed tunnel of the pressure distribution on five non lifting bodies of revolution of different nose angles at zero incidences. The tests were made at Mach numbers of 2.45 and 3.19. The results are compared with the pressure distributions given by two approximate theoretical methods, and good agreement is found at the Mach numbers used.	en_UK
dc.language.iso	en	en_UK
dc.publisher	College of Aeronautics, Cranfield	en_UK
dc.relation.ispartofseries	College Reports	en_UK
dc.relation.ispartofseries	79	en_UK
dc.title	An experimental investigation of the pressure distributions on five bodies of revolution at Mach numbers of 2.45 and 3.19	en_UK
dc.type	Report	en_UK