[
[1] Liersch, C. M., Hepperle M. 2011, “A distributed toolbox for multidisciplinary preliminary aircraft design”, CEAS Aeronautical Journal, pp. 57-68, 2011.10.1007/s13272-011-0024-6
]Search in Google Scholar
[
[2] “AGILE - Aircraft 3rd Generation MDO for Innovative Collaboration of Heterogeneous Teams of Experts“, [Online]. Available: http://www.agile-project.eu/.
]Search in Google Scholar
[
[3] “SimSAC project flyer,” [Online]. Available: http://www.transport-research.info/sites/default/files/project/documents/20120921_105849_29226_SimSAC-Flyer.pdf.
]Search in Google Scholar
[
[4] Kesseler E., Guenov M, 2010, “Advances in Collaborative Civil Aeronautical Multidisciplinary Design Optimization”, American Institute of Aeronautics and Astronautics.10.2514/4.867279
]Search in Google Scholar
[
[5] Baalbergen E., Kanakis A., Vankan W., 2009, “A practical approach for coordination of multi-partner engineering jobs in the design of small aircraft”, CESAR Special Issue of Journal Czech Aerospace Proceedings, vol. 3.
]Search in Google Scholar
[
[6] Coleman P., 2012, “Innovations in collaborative modelling and simulation to deliver the Behavioural Digital Aircraft, CRESCENDO Forum Participants Handbook.”, Toulouse.
]Search in Google Scholar
[
[7] TOICA Consortium, “EU FP7 TOICA Project public web page”, [Online]. Available: http://www.toica-fp7.eu/.
]Search in Google Scholar
[
[8] Sobieszczanski-Sobieski, J., 1995, “Multidisciplinary Design Optimization: An Emerging New Engineering Discipline”, Advances in Structural Optimization, pp. 483-496.10.1007/978-94-011-0453-1_14
]Search in Google Scholar
[
[9] Martins, J. R., Lambe, A. B., 2013, “Multidisciplinary Design Optimization: A Survey of Architectures”, AIAA Journal, 9(51), pp. 2049-2075.10.2514/1.J051895
]Search in Google Scholar
[
[10] Liscouët-Hanke, S., 2008, “A Model-Based Methodology for Integrated Preliminary Sizing and Analysis of Aircraft Power System Architectures”, Doctoral Thesis.
]Search in Google Scholar
[
[11] Scholz, D., 2009, “Aircraft Systems Overview - Greening of Secondary Power Systems”, SWAFEA - Sustainable Way for Alternative Fuels and Energy for Aviation, Brussels, Belgium, 23-24 April 2009.
]Search in Google Scholar
[
[12] Scholz, D., 2002, “Aircraft Systems - Reliability, Mass, Power and Costs”, EWADE.
]Search in Google Scholar
[
[13] Chakraborty, I., Mavris, D. N., 2016, “Integrated Assessment of Aircraft and Novel Subsystem Architectures in Early Design”, AIAA SciTech.10.2514/6.2016-0215
]Search in Google Scholar
[
[14] Martins Pires, R. M., Lajux, V., Fielding, J. P., 2016, “Methodology for the design and evaluation of wing leading edge and trailing edge devices”, ICAS, Hamburg, Germany.
]Search in Google Scholar
[
[15] Raymer, D.P., 2012, “Aircraft Design: A Conceptual Approach (5thEdition)“, American Institute of Aeronautics and Astronautics, Washington, DC.10.2514/4.869112
]Search in Google Scholar
[
[16] Roskam, J., 2003, “Airplane Design Part I: Preliminary Sizing of Airplanes (2ndEdition)“, DARcorporation, Lawrence, KS.
]Search in Google Scholar
[
[17] Torenbeek, E., 1976, “Synthesis of subsonic airplane design“, Nijgh-Wolters-Noordhoff, Rotterdam.
]Search in Google Scholar
[
[18] Fioriti, M., 2014, “Adaptable conceptual aircraft design model”, Advances In Aircraft and Spacecraft Science, vol. 1, pp. 43-67.10.12989/aas.2014.1.1.043
]Search in Google Scholar
[
[19] Rosero, J. A., Ortega, J. A., Aldabas, E., 2007, “Moving towards a more electric aircraft”, IEEE Aerospace and Electronic Systems Magazine, vol. 22, n. 3, pp. 3-9.10.1109/MAES.2007.340500
]Search in Google Scholar
[
[20] Jones, R. I., 2002, “The more electric aircraft - assessing the benefits”, Proceedings of the Institution of Mechanical Engineers, Part G Journal of Aerospace Engineering, vol. 216, pp. 259-269.10.1243/095441002321028775
]Search in Google Scholar
[
[21] Berlowitz, I., 2010, “All/More Electric Aircraft Engine & Airframe Systems Implementation”, The 9th Israeli Symposium on Jet Engines and Gas Turbines.
]Search in Google Scholar
[
[22] Heney, P. J., 2002, “A380 pushes 5000 psi into realm of the common man”, Hydraulics & Pneumatics.
]Search in Google Scholar
[
[23] Longxian, X., 2009, “Actuation technology for Flight Control System - Master Thesis”, Cranfield University.
]Search in Google Scholar
[
[24] Van Den Bossche, D., 2006, “The A380 flight control electrohydrostatic actuators, achievements and lessons learnt”, ICAS, Hamburg, Germany.
]Search in Google Scholar
[
[25] Tagge, G. E., Irish L. A., Bailey, A. R., 1985, “Systems Study for an Integrated Digital/Electric Aircraft (IDEA)”, NASA Contractor Report 3840, Hampton (VA).
]Search in Google Scholar
[
[26] Sinnet, M., 2007, “787 No-Bleed Systems: Saving Fuel and Enhancing Operational Efficiencies”, Aero Quarterly QTR_04 | 07, 06-11.
]Search in Google Scholar
[
[27] Mecham, M., 2005, “Boeing 787 Technology. Evolution and revolution”, Aviation week & Space technology, vol. 162, n. 13, pp. 46-50.
]Search in Google Scholar
[
[28] Baird, F., 2015, “Dreamliner Cabin Pressure Tech Reduces Altitude Sickness, Benefits PaxEx”, Airline passenger experience, apex association.
]Search in Google Scholar
[
[29] Meier O. e Scholz D., 2010, “A handbook method for the estimation of power requirements for electrical de-icing systems”, Aero - Aircraft Design and Systems Group.
]Search in Google Scholar
[
[30] Ciampa, P. D., Nagel, B., 2016, “Towards the 3rd generation MDO collaborative environment”, ICAS.
]Search in Google Scholar