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References Konstantinos G. Kyprianidis [8] A.H. Lefebvre. Gas Turbine Combustion. Taylor & Francis, PA, USA, 2nd edition, 1999. [9] R.W. Claus, A.L. Evans, J.K. Lylte, and L.D. Nichols. Numerical Propul- sion System Simulation. Computing Systems in Engineering (ISSN 0956- 0521), 2(4):357–364, 1991. [10] J.K. Lytle. The Numerical Propulsion System Simulation: An Overview. NASA/TM2000-209915, NASA Glenn Research Center, June 2000. [11] E. Onat and G. W. Klees. A method to estimate weight and dimensions of large and small gas turbine engines. NASA-CR-159481, NASA, January 1979. [12] M.T. Tong, I. Halliwell, and L.J. Ghosn. A computer code for gas turbine engine weight and disk life estimation. ASME Journal of Engineering for Gas Turbines and Power, 126(2):265–270, April 2004. [13] M.T. Tong and B.A. Naylor. An Object-Oriented Computer Code for Aircraft Engine Weight Estimation. In ASME TURBO EXPO 2008 Pro- ceedings, GT2008-50062, Berlin, Germany, June 2008. [14] L.A. McCullers. Aircraft configuration optimization including optimized flight profiles. In NASA Symposium on Recent Experiences in Multidisci- plinary Analysis and Optimization, NASA-CP-2327, Part 1, pp. 395-412, Hampton, Virginia, USA, April 1984. [15] K. Kontos, B. Janardan, and P. Gliebe. Improved NASA-ANOPP Noise Prediction Computer Code for Advanced Subsonic Propulsion Systems. NASA-CR-195480, NASA Lewis Research Center, Cleveland, OH, USA, August 1996. [16] N. Antoine, I. Kroo, K. Willcox, and G. Barter. A Framework for Air- craft Conceptual Design and Environmental Performance Studies. In 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Confer- ence Proceedings, AIAA 2004-4314, Albany, New York, September 2004. [17] C.R. Mercer, W.J. Haller, and M.T. Tong. Adaptive Engine Technologies for Aviation CO2 Emissions Reduction. In 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA20065105, Sacramento, California, USA, July 2006. 182PDF Image | Multi-disciplinary conceptual design of future jet engine systems
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