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Konstantinos G. Kyprianidis References [40] S.H. Lee, M. Le Dilosquer, R. Singh, S.E. Hobbs, C. Giannakopoulos, P.H. Plantevin, K.S. Law, J.A. Pyle, and M.J. Rycroft. Implications of NOy emissions from subsonic aircraft at cruise altitude. Proceedings of the Insti- tution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 211(3):157–168, 1997. [41] S. Gayraud. Technical and Economical Assessment for Industrial Gas Tur- bine Selection. Master’s thesis, Cranfield University, Cranfield, Bedford- shire, United Kingdom, 1996. [42] S. Gayraud. Design of a Decision Support System for Combined Cy- cle Schemes. MPhil thesis, Cranfield University, Cranfield, Bedfordshire, United Kingdom, 1998. [43] M.W. Whellens and R. Singh. Propulsion System Optimisation for Min- imum Global Warming Potential. In 23rd ICAS Congress Proceedings, Toronto, Canada, September 2002. [44] M.W. Whellens, H. Taguchi, R. Singh, and P. Pilidis. Genetic Algorithm Based Optimisation of Intercooled Recuperated Turbofan Desgin. In 41st AIAA Aerospace Sciences Meeting and Exhibit Proceedings, Reno, Nevada, USA, January 2003. [45] M.W. Whellens. Multidisciplinary Optimisation of Aero-Engines Using Genetic Algorithms and Preliminary Design Tools. PhD thesis, Cranfield University, Cranfield, Bedfordshire, United Kingdom, 2003. [46] F. Svensson. Potential of Reducing the Environmental Impact of Civil Sub- sonic Aviation by Using Liquid Hydrogen. PhD thesis, Cranfield University, Cranfield, Bedfordshire, United Kingdom, 2005. [47] F. Svensson, A. Hasselrot, and J. Moldanova. Reduced environmen- tal impact by lowered cruise altitude for liquid hydrogen-fuelled aircraft. Aerospace Science and Technology, 8(4):307–320, June 2004. [48] T. Papadopoulos. Gas Turbine Cycles for Intermediate Load Power Gen- eration. PhD thesis, Cranfield University, Cranfield, Bedfordshire, United Kingdom, 2005. 185PDF Image | Multi-disciplinary conceptual design of future jet engine systems
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