Use this URL to cite or link to this record in EThOS: http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.344070
Title: Heat transfer and fluid flow in the high pressure compressor drive cone cavity of an aeroengine.
Author: Kais, G.
Awarding Body: University of Sussex
Current Institution: University of Sussex
Date of Award: 1998
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Abstract:
No abstract available
Supervisor: Not available Sponsor: Not available
Qualification Name: Thesis (Ph.D.) Qualification Level: Doctoral
EThOS ID: uk.bl.ethos.344070  DOI: Not available
Keywords: Gas turbine engines; Rolls Royce; Design Aerodynamics Jet engines Gas-turbines Airplanes
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