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

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dc.contributor.authorMarson, G. B.
dc.contributor.authorSocha, W.
dc.contributor.authorKeates, R. E.
dc.date.accessioned2012-09-11T15:40:47Z
dc.date.available2012-09-11T15:40:47Z
dc.date.issued1954-04
dc.description.abstractMeasurements 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.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/7565
dc.language.isoenen_UK
dc.publisherCollege of Aeronautics, Cranfielden_UK
dc.relation.ispartofseriesCollege Reportsen_UK
dc.relation.ispartofseries79en_UK
dc.titleAn experimental investigation of the pressure distributions on five bodies of revolution at Mach numbers of 2.45 and 3.19en_UK
dc.typeReporten_UK

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