The free streamline method applied to the flow at the rear of a duct

Craven, A. H.

dc.contributor.author	Craven, A. H.
dc.date.accessioned	2013-06-19T15:30:49Z
dc.date.available	2013-06-19T15:30:49Z
dc.date.issued	1956-03
dc.identifier.uri	http://dspace.lib.cranfield.ac.uk/handle/1826/7968
dc.description.abstract	The free streamline technique is extended to the problem of two-dimensional jet flow from the rear of a nacelle. Complex potentials for the jet flow and the flow in the free stream are found and from these the equation of the wake streamline and the velocity and pressure distributions are calculated. some consideration is also given to the corresponding axi-symmetric problem.	en_UK
dc.language.iso	en	en_UK
dc.publisher	College of Aeronautics, Cranfield	en_UK
dc.relation.ispartofseries	College Report	en_UK
dc.relation.ispartofseries	99	en_UK
dc.title	The free streamline method applied to the flow at the rear of a duct	en_UK
dc.type	Report	en_UK