The effect of nozzle exit geometry on the aerodynamic performance of bypass flow of turbofan engines

Bibliographic Details
Main Author:	Sloan, B.
Published:	Queen's University Belfast 2009
Subjects:	629.13
Online Access:	http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.517527

id	ndltd-bl.uk-oai-ethos.bl.uk-517527
record_format	oai_dc
spelling	ndltd-bl.uk-oai-ethos.bl.uk-5175272015-03-20T04:54:10ZThe effect of nozzle exit geometry on the aerodynamic performance of bypass flow of turbofan enginesSloan, B.2009629.13Queen's University Belfasthttp://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.517527Electronic Thesis or Dissertation
collection	NDLTD
sources	NDLTD
topic	629.13
spellingShingle	629.13 Sloan, B. The effect of nozzle exit geometry on the aerodynamic performance of bypass flow of turbofan engines
author	Sloan, B.
author_facet	Sloan, B.
author_sort	Sloan, B.
title	The effect of nozzle exit geometry on the aerodynamic performance of bypass flow of turbofan engines
title_short	The effect of nozzle exit geometry on the aerodynamic performance of bypass flow of turbofan engines
title_full	The effect of nozzle exit geometry on the aerodynamic performance of bypass flow of turbofan engines
title_fullStr	The effect of nozzle exit geometry on the aerodynamic performance of bypass flow of turbofan engines
title_full_unstemmed	The effect of nozzle exit geometry on the aerodynamic performance of bypass flow of turbofan engines
title_sort	effect of nozzle exit geometry on the aerodynamic performance of bypass flow of turbofan engines
publisher	Queen's University Belfast
publishDate	2009
url	http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.517527
work_keys_str_mv	AT sloanb theeffectofnozzleexitgeometryontheaerodynamicperformanceofbypassflowofturbofanengines AT sloanb effectofnozzleexitgeometryontheaerodynamicperformanceofbypassflowofturbofanengines
_version_	1716787156700102656

The effect of nozzle exit geometry on the aerodynamic performance of bypass flow of turbofan engines

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