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References Konstantinos G. Kyprianidis [211] [212] [213] [214] [215] [216] [217] [218] [219] [220] L. Xu and T. Gro ̈nstedt. Design and Analysis of an Intercooled Turbofan Engine. ASME Journal of Engineering for Gas Turbines and Power, GTP- 09-1228, in press, December 2009. A.D. Walker, J.F. Carrotte, and A.M. Rolt. Duct Aerodynamics for Inter- cooled Aero Gas Turbines: Constraints, Concepts and Design Methododol- ogy. In ASME TURBO EXPO 2009 Proceedings, GT2009-59612, Orlando, Florida, June 2009. A. Lundbladh and A. Sjunnesson. Heat Exchanger Weight and Efficiency Impact on Jet Engine Transport Applications. In ISABE 2003 Proceedings, ISABE-2003-1122, Cleveland, USA, September 2003. G. Pellischek and B. Kumpf. Compact Heat Exchanger Technology for Aero Engines. In ISABE 1991 Proceedings, ISABE-91-7019, Nottingham, United Kingdom, September 1991. H. Schoenenborn, E. Ebert, B. Simon, and P. Storm. Thermomechanical Design of a Heat Exchanger for a Recuperated Aeroengine. ASME Journal of Engineering for Gas Turbines and Power, 128(4):736–744, October 2006. C.F. McDonald, A. Massardo, C. Rodgers, and A. Stone. Recuperated gas turbine aeroengines, part I: early development activities. Aircraft Engineer- ing and Aerospace Technology: An International Journal, 80(2):139–157, 2008. C.F. McDonald, A. Massardo, C. Rodgers, and A. Stone. Recuperated gas turbine aeroengines, part II: engine design studies following early de- velopment testing. Aircraft Engineering and Aerospace Technology: An International Journal, 80(3):280–294, 2008. C.F. McDonald, A. Massardo, C. Rodgers, and A. Stone. Recuperated gas turbine aeroengines, part III: engine concepts for reduced emissions, lower fuel consumption, and noise abatement. Aircraft Engineering and Aerospace Technology: An International Journal, 80(4):408–426, 2008. A.M. Rolt. UK Patent GB 2 413 366 B, September 2006. D.E. Gray and J.W. Witherspoon. Fuel conservative propulsion concepts for future air transports. Technical Report SAE-760535, Society of Auto- motive Engineers, 1976. 202PDF Image | Multi-disciplinary conceptual design of future jet engine systems
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