[
[1] Austyn-Mair, W. and Birdsall, David L. Aircraft Performance. 1st ed. Vol. 5. Cambridge Aerospace Series. Cambridge University Press. Cambridge, United Kingdom (1992). ISBN: 0521568366.
]Search in Google Scholar
[
[2] Bartel, Matthias and Young, Trevor. “Simplified Thrust and Fuel Consumption Models for Modern Two-Shaft Turbofan Engines.” Journal of Aircraft J AIRCRAFT 45 (July 2008), pp. 1450–1456. DOI: 10.2514/1.35589.
]Open DOISearch in Google Scholar
[
[3] Department of Transportation Federal Aviation Administration. “Electronic Code of Federal Regulations Title 14 Part 25.” Online. Airworthiness Standards: Transport Category Airplanes. Washington DC. (2016).
]Search in Google Scholar
[
[4] “Flightpath 2050: Europe’s Vision for Aviation.” European Commission, Luxembourg. (2011). ISBN: 9789279197246.
]Search in Google Scholar
[
[5] Gudmundsson, Snorri. General Aviation Aircraft Design: Applied Methods and Procedures. 1st ed. Elsevier Inc, Oxford UK (2014). ISBN: 9780123973085.
]Search in Google Scholar
[
[6] Heffley, R. K. and Jewell, W. F. “Aircraft handling qualities data.” Tech. rep. NASA CR-2144. National Aeronautics and Space Administration. Washington D.C. (1972).
]Search in Google Scholar
[
[7] Howe, Denis. Aircraft Conceptual Design Synthesis. Vol. 5. Aerospace Series. Wiley (2000). ISBN: 9781860583018.10.1002/9781118903094
]Search in Google Scholar
[
[8] Karpuk, Stanislav and Elham, Ali. “Conceptual Design Trade Study for an Energy-Efficient Mid-Range Aircraft with Novel Technologies”. AIAA Scitech. (2021). DOI: 10.2514/6.2021-0013.
]Open DOISearch in Google Scholar
[
[9] Mattingly, Jack D. Aircraft Engine Design. AIAA Education Series. American Institute of Aeronautics and Astronautics, Inc. (2018). ISBN: 978162 4105173.
]Search in Google Scholar
[
[10] Raymer, Daniel P. Aircraft Design: A Conceptual Approach. 6th ed. AIAA Education Series. American Institute of Aeronautics and Astronautics, Inc. Virginia, U.S.A. (2018). ISBN: 9781624104909.10.2514/4.104909
]Search in Google Scholar
[
[11] Roskam, Jan. Airplane Design Part VI: Preliminary Calculation of Aerodynamic, Thrust and Power Characteristics. Design, Analysis and Research Corporation. Kansas, U.S.A: (2004). ISBN: 1884885527.
]Search in Google Scholar
[
[12] Roskam, Jan. Airplane Flight Dynamics and Automatic Flight Controls. 1st ed. Vol. 1. Design, Analysis and Research Corporation. Kansas, U.S.A. (1995). ISBN: 1884885179.
]Search in Google Scholar
[
[13] Sadraey, Mohammad H. Aircraft Performance: An engineering approach. CRC Press, FL (2016). ISBN: 9781498776554.10.1201/9781315366913
]Search in Google Scholar
[
[14] Schmidt, Louis V. Introduction to Aircraft Flight Dynamics. Vol. 1. American Institute of Aeronautics and Astronautics, Inc. VA, USA. (1998). ISBN: 1563472260.
]Search in Google Scholar
[
[15] Scholtz, Dieter. Aircraft design notes: 5. preliminary sizing. (2015) https://www.fzt.haw-hamburg.de/pers/Scholz/HOOU/AircraftDesign_5_preliminarySizing.pdf
]Search in Google Scholar
[
[16] Lukaczyk, Trent W., Wendorff, Andrew D., Colonno, Michael, Economon, Thomas D., Alonso, Juan J., Orra, Tarik H., and Ilario, Carlos. “SUAVE: An Open-Source Environment for Multi-Fidelity Conceptual Vehicle Design”. Proceedings of the 16th AIAA ISSMO Multidisciplinary Analysis and Optimization Conference pp. 1–9. (22-26 2015). DOI: 10.2514/6.2015-3087.
]Open DOISearch in Google Scholar
[
[17] Torenbeek, Egbert. Synthesis of Subsonic Airplane Design. Kluwer Academic Publishers. Dordrecht, The Netherlands (1986). ISBN: 9024727243.
]Search in Google Scholar
[
[18] Department of Defense, United States of America. “Military Specification: Flying Qualities of Piloted Airplanes.” MIL-F-8785C. (1980).
]Search in Google Scholar
, 