Aircraft Conceptual Optimization Research Articles

Numerical Evaluation of Airfoil Friction Drag

7Torenbeek, E., Synthesis of SubsonicAirplaneDesign, Delft Univ. Press, Kluwer Academic, Norwell, MA, 1982, pp. 167–170, 263–294, 445–465, 487–556. 8Raymer, D. P., Aircraft Design: A Conceptual Approach, AIAA Education Series, AIAA, Washington, DC, 1989, pp. 391–405. 9Crossley, W. A., and Laananen, D. H., “Conceptual Design of Helicopters via Genetic Algorithm,” Journal of Aircraft, Vol. 33, No. 6, 1996, pp. 1062–1070. 10Crispin, Y., “Adaptive Conceptual Optimization of General Aviation Aircraft,” AIAA Paper 92-4195,Aug. 1992. 11Crispin, Y., “Aircraft Conceptual Optimization using Simulated Evolution,” AIAA Paper 94-0092, Jan. 1994. 12Bramlette, M. F., and Cusic, R., “A Comparative Evaluation of Search Methods Applied to Parametric Design of Aircraft,” Proceedings of the 3rd International Conference on Genetic Algorithms, Morgan Kaufmann, San Mateo, CA, 1989, pp. 213–238. 13Roth, G. L., and Crossley, W. A., “Conceptual Design of a Commercial Transport Aircraft Using a Genetic Algorithm-Based Approach,” AIAA Paper 98-4934, Sept. 1998. 14Roskam, J., Airplane Design—Part VIII, Roskam Aviation and Engineering Corp., Kansas, 1988, Chap. 5, pp. 80–109. 15Goldberg, D. E., Genetic Algorithms in Search, Optimization and Machine Learning, Addison Wesley Longman, Reading, MA, 1989, pp. 59– 88.