References

  • [Anderson, 2001] Anderson, J. D., “Fundamentals of aerodynamics, 2001,” .
  • [Burton, 2017] Burton, M., Solar-Electric and Gas Powered, Long-Endurance UAV Sizing via Geometric Programming, Master’s thesis, Massachusetts Institute of Technology, Cambridge, MA, 2017.
  • [Chai, 1996] Chai, S. T. and Mason, W. H., Landing gear integration in aircraft conceptual design, Master’s thesis, Virginia Polytechnic Institute and State University, 1996.
  • [Currey, 1984] Currey, N. S., Landing Gear Design Handbook, Lockheed-Georgia Company, 1984.
  • [Drela, 1989] Drela, M., “XFOIL: An analysis and design system for low Reynolds number airfoils,” Low Reynolds number aerodynamics, Springer, 1989, pp. 1–12.
  • [Drela, 2011] Drela, M., TASOPT 2.08 Transport Aircraft System OPTimization, 2011.
  • [Hoburg, 2013] Hoburg, W. and Abbeel, P., “Geometric programming for aircraft design optimization,” AIAA Journal, Vol. 52, No. 11, 2014, pp. 2414–2426.
  • [Hoburg, 2014] Hoburg, W., Kirschen, P., and Abbeel, P., “Fitting Geometric Programming Models to Data,” Optimization and Engineering.
  • [Kirschen, 2016] ] Kirschen, P. G., Signomial Programming for Aircraft Design, Master’s thesis, Massachusetts Institute of Technology, Cambridge, MA, 2016.
  • [Kroo, 2001] Kroo, I., Altus, S., Braun, R., Gage, P., and Sobieski, I., “Multidisciplinary optimization methods for aircraft preliminary design,” AIAA paper, Vol. 4325, 1994, pp. 1994.
  • [Nita, 2012] Nita, M. and Scholz, D., Estimating the oswald factor from basic aircraft geometrical parameters, Deutsche Gesellschaft für Luft-und Raumfahrt-Lilienthal-Oberth eV, 2012.
  • [Raymer, 1992] Raymer, D. P., “Aircraft Design: A Conceptual Approach,” 1992.
  • [Torenbeek, 1982] Torenbeek, E., Synthesis of subsonic aircraft design, 1982.
  • [York, 2017] Martin York, W. H. and Drela, M., “Turbofan Engine Sizing and Tradeoff Analysis via Signomial Programming,” AIAA Journal of Aircraft, 2017.