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[4] Gorissen, D., Quaranta, E., Ferraro, M., Schumann, B., van Schaik, J., Gisbert, M.B.I., Keane, A., and Scanlan, J. (2014) Value-based decision environment: vision and application. J. Aircr., 51 (5), 1360-1372.

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Small Unmanned Fixed-wing Aircraft Design: A Practical Approach, First Edition. Andrew J. Keane, Andras Sobester and James P. Scanlan.

© 2017 John Wiley & Sons Ltd. Published 2017 by John Wiley & Sons Ltd.

[15] Gudmundsson, S. (2014) General Aviation Aircraft Design, Butterworth-Heinemann, Oxford.

[16] Koza, J. (1992) Genetic Programming: On the Programming of Computers by Means of Natural Selection, MIT Press, Cambridge, MA.

[17] Sobester, A. (2014) Four Suggestions for Better Parametric Geometries. 10th AIAA Multidisciplinary Design Optimization Conference, National Harbor, MD.

[18] Gundlach, J. (2012) Designing Unmanned Aircraft Systems: A Comprehensive Approach, AIAA, Reston, VA.

[19] Anderson, J.D. Jr. (2011) Introduction to Flight, 7th edn, McGraw Hill, New York.

[20] Abbott, I.H. and von Doenhoff, A.E. (1959) Theory of Wing Sections: Including a Summary of Airfoil Data, Dover Publications, New York.

[21] Sivells, J.C. and Spooner, S.H. (1949) Investigation in the Langley 19-Foot Pressure Tunnel of Two Wings of NACA 65-210 and 64-210 Airfoil Sections with Various Type Flaps. Technical report 942, NACA.

[22] Gentry, G.L., Bezos, G.M., Dunham, R.E. Jr., and Melson, W.E. Jr. Wind Tunnel Aerodynamic Characteristics of a Transport-Type Airfoil in a Simulated Heavy Rain Environment. Nasa-cr-181119, NASA, 1992.

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[26] Mader, C.A. and Martins, J. (2011) Computation of aircraft stability derivatives using an automatic differentiation adjoint approach. AIAA J., 49, 2737-2750.

[27] Golland, L. (1952) Aileron Reversal of Straight and Swept Wings at High Subsonic Speeds. Technical report 52-231, Wright Air Development Center.

[28] Karuzic, F.G. (2007) Conceptual design of silent and green airliners. Msc thesis. Cranfield.

 
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