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Multi-disciplinary conceptual design of future jet engine systems

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Multi-disciplinary conceptual design of future jet engine systems ( multi-disciplinary-conceptual-design-future-jet-engine-syste )

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References Konstantinos G. Kyprianidis [87] Society of Automotive Engineers. Gas Turbine Engine Performance Pre- sentation and Nomenclature for Digital Computers Using Object-Oriented Programming. SAE ARP 5571 Draft 6.0, Warrendale, PA, USA, August 2004. [88] P.P. Walsh and P. Fletcher. Gas Turbine Performance. Blackwell Science, United Kingdom, 1st edition, 1998. [89] RTO Applied Vehicle Technology Panel Task Group AVT-036. Perfor- mance Prediction and Simulation of Gas Turbine Engine Operation for Aircraft, Marine, Vehicular, and Power Generation. RTO-TR-AVT-036, NATO, France, February 2007. [90] P. Pilidis. Digital Simulation of Gas Turbine Performance. PhD thesis, University of Glasgow, Glasgow, United Kingdom, 1983. [91] A.A. Sirinoglou. Implementation of Variable Geometry for Gas Turbine Performance Simulation Turbomatch Improvement. Master’s thesis, Cran- field University, Cranfield, Bedfordshire, United Kingdom, 1992. [92] J. Kurzke. Performance modeling methodology: Efficiency definitions for cooled single and multistage turbines. In ASME TURBO EXPO 2002 Proceedings, 2002-GT-30497, Amsterdam, The Netherlands, June 2002. [93] R.E. Grey and H.D. Wilsted. Performance of Conical Jet Nozzles in Terms of Flow. NACA-TN-1757, NACA Lewis Flight Propulsion Laboratory, Cleveland, OH, USA, November 1948. [94] J. Kurzke. How to Get Component Maps for Aircraft Gas Turbine Perfor- mance Calculations. In ASME TURBO EXPO 1996 Proceedings, 96-GT- 164, Birmingham, U.K, June 1996. [95] J. Kurzke. Gas Turbine Performance Simulation with GasTurb 10. http://www.gasturb.de, 2007. [96] National Oceanic and Atmospheric Administration. U.S. Standard Atmo- sphere, 1976. USGPO-1976-O-588-286, National Aeronautics and Space Administration, U.S. Government Printing Office, Washington, D.C., USA, October 1976. 190

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