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Acknowledgments The work presented in this thesis has been performed under the project NEWAC (European Commission Contract No. AIP5-CT-2006-030876) and this funding is gratefully acknowledged. In more detail, the work was performed under NEWAC WP1.3, “Techno-Economic and Environmental Risk Analysis”, in close collabo- ration with L. Xu (Chalmers University), A. Alexiou (National Technical Univer- sity of Athens), and B. Lehmayr (University of Stuttgart). Their contributions in developing the NEWAC TERA2020 framework is acknowledged, and their support in the work presented in this thesis is much appreciated. I am indebted to Prof. P. Pilidis, Dr. S.O.T. Ogaji and Prof. R. Singh for many reasons; for giving me the opportunity to work at the Department of Power and Propulsion, for their continuous guidance in my research, but above all for encouraging me to be creative. Many thanks go to G. Hargreaves, M. Ne- gus, N. Datt, S. Broe, and L. Pearson for providing solutions to many admin- istrative problems. I would also like to express my most sincere gratitude to Prof. T. Gr ̈onstedt, Prof. L. Davidson, M. Vargman, and all my friends and col- leagues at Chalmers University for providing a friendly and stimulating working environment, and making my 6-month visit there an unforgettable experience. I am grateful to A.M. Rolt (Rolls-Royce) for providing a valuable insight on conceptual design and intercooled core benefits, as well as for his constructive suggestions on improving TERA2020 and for peer-reviewing the contents of this thesis. Many thanks also go to Prof. A.I. Kalfas for inspiring me to learn more about aero engines, for his encouragement and help in starting this PhD, and for his continuous support in my professional development over the past few years. I would like to express my appreciation to the reviewers of this work for their constructive suggestions on improving the overall quality and clarity of the thesis and resulting publications. Many thanks go to J.A. Borradaile for the numerous discussions and constructive suggestions which helped put much of his exper- tise into the TERA2020 tool conceptual design algorithm. Many thanks go to S. Bake (Rolls-Royce Deutschland) for his continuous support on conventional vPDF Image | Multi-disciplinary conceptual design of future jet engine systems
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