Desktop version

Home arrow Engineering arrow Small Unmanned Fixed-Wing Aircraft Design. A Practical Approach

V Bibliography

[1] Torenbeek, E. (1982) Synthesis of Subsonic Airplane Design, Kluwer Academic Publishers, Dordrecht, ISBN: 90-247-2724-3.

[2] van Schaik, J.R., Scanlan, J.P., Keane, A.J., Takeda, K., and Gorissen, D. (2011) Improving design rationale capture during embodiment design, in Proceedings of International Conference on Engineering Design, ICED11 (eds T. Howard, K. Mougaard, T. McAloone, and C. Hansen), The Design Society, pp. 436-445, ISBN: 978-1-904670-32-2.

[3] Gorissen, D., Quaranta, E., Ferraro, M., Scanlan, J., Keane, A., and Takeda, K. (2012) Architecting a Decision Environment for Complex Design Evaluation. Proceedings of the 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Honolulu, AIAA-2012-1806, doi: 10.2514/6.2012-1806.

[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.

[5] Stinton, D. (1983) The Design of the Aeroplane, Blackwell Science, Oxford, ISBN: 0-632-01877-1.

[6] Cousin, J. and Metcalf, M. (1990) The BAE (Commercial Aircraft) LTD Transport Aircraft Synthesis and Optimization Program. AIAA/AHS/ASEE Aircraft Design, Systems and Operations Conference, AIAA 90-3295, Dayton.

[7] Keane, A.J. (2003) Wing optimization using design of experiment, response surface, and data fusion methods. J. Aircr., 40 (4), 741-750.

[8] Walsh, J., Townsend, J., Salas, A., Samareh, J., Mukhopadhyay, V., and Barthelemy, J.-F. (2000) Multidisciplinary High-Fidelity Analysis and Optimization of Aerospace Vehicles, Part 1: Formulation. Proceedings of the 38th Aerospace Sciences Meeting and Exhibit. AIAA 2000-0418, Reno, NV.

[9] Hoerner, S.F. (1992) Fluid-Dynamic Drag, Hoerner Fluid Dynamics, Bakersfield, CA.

[10] Hoerner, S.F. (1992) Fluid-Dynamic Lift, Hoerner Fluid Dynamics, Bakersfield, CA.

[11] Raymer, D. (2012) Aircraft Design: A Conceptual Approach, AIAA Education Series, 3rd edn, AIAA.

[12] Brandt, J.B. and Selig, M.S. (2011) Propeller Performance Data at Low Reynolds Numbers. Proceedings of the 49th AIAA Aerospace Sciences Meeting, Orlando, AIAA-2011-1255.

[13] Falk, M. and Logan, G. (2002) Systems Engineering and Open Systems, SYS-301, Defense Acquisition University.

[14] ACSYNT (1995) ACSYNT: Installation Manual and User Guide, Version 3.0, ACSYNT Institute, Virginia Polytechnic Institute and State University, Blacksburg, VA 24061-0002.

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.

[23] Etkin, B. and Reid, L.D. (1996) Dynamics of Flight Stability and Control, 3rd edn, John Wiley & Sons, Inc., New York.

[24] Phillips, W. (2000) Improved closed-form approximation for Dutch roll. Journal of Aircr., 37, 484-490.

[25] Phillips, W. (2000) Phugoid approximation for conventional airplanes. J. Aircr., 37, 30-36.

[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.

< Prev   CONTENTS   Source

Related topics