Please use this identifier to cite or link to this item: http://dspace.unimap.edu.my:80/xmlui/handle/123456789/21041
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dc.contributor.authorHamdani, Hamid-
dc.date.accessioned2012-09-25T04:35:46Z-
dc.date.available2012-09-25T04:35:46Z-
dc.date.issued2009-
dc.identifier.urihttp://dspace.unimap.edu.my/123456789/21041-
dc.descriptionAccess is limited to UniMAP community.en_US
dc.description.abstractThis analysis focuses on the evaluation and analysis of thermal Brayton, Ericsson, and Rankine cycle. Under the examined conditions, the thermal efficiency, the exergy efficiency and power produced for each cycle should be calculated and analyzed. Production of power in space for terrestrial use is of great interest in view of the rapidly rising power demand. Space can be the most interesting area that can be discovered because space can offer very low temperature that cannot be offered by the earth surface. This analysis also used different types of fluids for all cycles which is argon(Ar), nitrogen(N2), argon-xenon(Ar-Xe), helium(He), helium-xenon(He-Xe), and hydrogen(H2). Only the first two fluids which is argon and nitrogen were considered for Rankine cycle.en_US
dc.language.isoenen_US
dc.publisherUniversiti Malaysia Perlisen_US
dc.subjectSpaceen_US
dc.subjectThermal cycles spaceen_US
dc.subjectThermodynamicsen_US
dc.subjectThermal power cyclesen_US
dc.titleAnalysis of thermal power cycles for use in spaceen_US
dc.typeLearning Objecten_US
dc.contributor.advisorGhulam Abdul Quadir, Prof. Madya Dr.en_US
dc.publisher.departmentSchool of Mechatronic Engineeringen_US
Appears in Collections:School of Mechatronic Engineering (FYP)

Files in This Item:
File Description SizeFormat 
Abstract, Acknowledgement.pdf159.97 kBAdobe PDFView/Open
Conclusion.pdf106.55 kBAdobe PDFView/Open
Introduction.pdf110.39 kBAdobe PDFView/Open
Literature review.pdf231.31 kBAdobe PDFView/Open
Methodology.pdf288.9 kBAdobe PDFView/Open
References and appendix.pdf344.26 kBAdobe PDFView/Open
Results and discussion.pdf364.28 kBAdobe PDFView/Open


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