[1] Ravi, B., Deo, J., Starnes, H., Richard, Jr., and Holzwarth, C., "Low-Cost Composite Materials and Structures for Aircraft Applications," Paper presented at the RTO AVT Specialists’ Meeting on “Low Cost Composite Structures”, held in Loen, Norway, 7-11 May 2001.
[2] Lolis, P., Development of a Preliminary Weight Estimation Method for Advanced Turbofan Engines, (Ph.D. Thesis), University of Craneld, 2014.
[3] Whitehead, L. T. and Brown., J., “A mechanical design for a lightweight turbo-jet engine and the variation of engine weight with size, “National gas turbine establishment, Memorandum M.177, August 1953.
[4] Pennington, W.A., “Choice of engines for aircraft”, Shell Aviation News, January 1959, pages 14-19.
[5] Guha, A., Boylan, D. and Gallagher, P., “Determination of optimum specic thrust for civil aero gas turbine engines: A multidisciplinary design synthesis and optimisation”, Part G: Journal of Aerospace Engineering, Vol. 227, No.3, 2012.
[6] Svoboda, C., “Turbofan engine database as a preliminary design tool”, Journal of Aircraft design, Vol.3, 2000, pp.17-31.
[7] Raymer, D. P., “Aircraft design: A conceptual approach”, AIAA, 1989.
[8] Jenkinson, L. R., Simpkin, P. and Rhodes, D., Civil Jet Aircraft Design, Butterwoth-Heinemann, 1999.
[9] Daly, M., editor. Jane's aero-engines. 28 rd Ed, IHS Janes, September 2010.
[10] Torenbeek., E., “Synthesis of Subsonic Airplane Design”, Martinus Nijhoff publishers, 1975.
[11] Clavier, J., Aero gas turbine engine design project (AVIC). Ultra high bypass ratio (12-14) study, (Master's Thesis), University of Craneld, 2008.
[12] Gerend, R. P. and Roundhill, J. P., "Correlation of gas turbine engine weights and dimensions," In Propulsion Joint Specialist Conference, AIAA,Vol. 669, 1970, pages 1-7.
[13] Colmenares Quintero, R.F., Techno-economic and enviromental risk assessment of innovative propulsion systems for short-range civil aircraft, (Ph.D. Thesis), University of Craneld, April 2009.
[14] Sagerser, D. A., Lieblein, S. and Krebs, R. P., “Empirical expressions for estimating length and weight of axial-ow components of VTOL powerplants," Technical Report TM X-2406, NASA, December 1971.
[15] Pera, R.J., Onat, E., Klees, G. W. and Tjonneland, E., “A method to estimate weight and dimensions of aircraft gas turbine engines." Vol. 1, Method of analysis nal report Technical Report NASA-CR-135170, NASA, 1977.
[16] G. W. Klees and L. Fishbach, H., “Aircraft engine weight estimation method," Proceedings of the thirty-seventh annual conference of the Society of Allied Weight Engineers, number 1248. SAWE, May 1978.
[17] Onat, E. and Tolle, F.F., “An extension of engine weight estimation techniques to compute engine production cost ,“Technical Report N62269-78-C-0286, Naval Air Development Center, 1979.
[18] Hale, P.L., “A method to estimate weight and dimensions of small aircraft propulsion gas turbine engines ,“Technical Report NASA-CR-168049, NASA - Garrett turbine engine company, 1982.
[19] Tong, M.T., Halliwell, I. and Ghosn, L. J., “A computer code for gas turbine engine weight and disk life estimation, “Journal of Engineering for Gas Turbines and Power, Vol.126, No. 2, 2004, pp.265-270.
[20] Tong, M. T. and Naylor, B. A., “An object-oriented computer code for aircraft engine weight estimation," In Proceedings of the ASME Turbo Expo, Vol. 1, 2008, pages 1-7.
[1] Ravi, B., Deo, J., Starnes, H., Richard, Jr., and Holzwarth, C., "Low-Cost Composite Materials and Structures for Aircraft Applications," Paper presented at the RTO AVT Specialists’ Meeting on “Low Cost Composite Structures”, held in Loen, Norway, 7-11 May 2001.
[2] Lolis, P., Development of a Preliminary Weight Estimation Method for Advanced Turbofan Engines, (Ph.D. Thesis), University of Craneld, 2014.
[3] Whitehead, L. T. and Brown., J., “A mechanical design for a lightweight turbo-jet engine and the variation of engine weight with size, “National gas turbine establishment, Memorandum M.177, August 1953.
[4] Pennington, W.A., “Choice of engines for aircraft”, Shell Aviation News, January 1959, pages 14-19.
[5] Guha, A., Boylan, D. and Gallagher, P., “Determination of optimum specic thrust for civil aero gas turbine engines: A multidisciplinary design synthesis and optimisation”, Part G: Journal of Aerospace Engineering, Vol. 227, No.3, 2012.
[6] Svoboda, C., “Turbofan engine database as a preliminary design tool”, Journal of Aircraft design, Vol.3, 2000, pp.17-31.
[7] Raymer, D. P., “Aircraft design: A conceptual approach”, AIAA, 1989.
[8] Jenkinson, L. R., Simpkin, P. and Rhodes, D., Civil Jet Aircraft Design, Butterwoth-Heinemann, 1999.
[9] Daly, M., editor. Jane's aero-engines. 28 rd Ed, IHS Janes, September 2010.
[10] Torenbeek., E., “Synthesis of Subsonic Airplane Design”, Martinus Nijhoff publishers, 1975.
[11] Clavier, J., Aero gas turbine engine design project (AVIC). Ultra high bypass ratio (12-14) study, (Master's Thesis), University of Craneld, 2008.
[12] Gerend, R. P. and Roundhill, J. P., "Correlation of gas turbine engine weights and dimensions," In Propulsion Joint Specialist Conference, AIAA,Vol. 669, 1970, pages 1-7.
[13] Colmenares Quintero, R.F., Techno-economic and enviromental risk assessment of innovative propulsion systems for short-range civil aircraft, (Ph.D. Thesis), University of Craneld, April 2009.
[14] Sagerser, D. A., Lieblein, S. and Krebs, R. P., “Empirical expressions for estimating length and weight of axial-ow components of VTOL powerplants," Technical Report TM X-2406, NASA, December 1971.
[15] Pera, R.J., Onat, E., Klees, G. W. and Tjonneland, E., “A method to estimate weight and dimensions of aircraft gas turbine engines." Vol. 1, Method of analysis nal report Technical Report NASA-CR-135170, NASA, 1977.
[16] G. W. Klees and L. Fishbach, H., “Aircraft engine weight estimation method," Proceedings of the thirty-seventh annual conference of the Society of Allied Weight Engineers, number 1248. SAWE, May 1978.
[17] Onat, E. and Tolle, F.F., “An extension of engine weight estimation techniques to compute engine production cost ,“Technical Report N62269-78-C-0286, Naval Air Development Center, 1979.
[18] Hale, P.L., “A method to estimate weight and dimensions of small aircraft propulsion gas turbine engines ,“Technical Report NASA-CR-168049, NASA - Garrett turbine engine company, 1982.
[19] Tong, M.T., Halliwell, I. and Ghosn, L. J., “A computer code for gas turbine engine weight and disk life estimation, “Journal of Engineering for Gas Turbines and Power, Vol.126, No. 2, 2004, pp.265-270.
[20] Tong, M. T. and Naylor, B. A., “An object-oriented computer code for aircraft engine weight estimation," In Proceedings of the ASME Turbo Expo, Vol. 1, 2008, pages 1-7.
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