Analysis of Axiomatic Design Influence on Aircraft Design Process

[1] W. Hsu and I. M. Woon, Current and Future Research in the Conceptual Design of Mechanical Products, Comput. Des., 30 (1998) 377-389.

[2] J. Sobieszczanski Sobieski, A. Morris, M. J. L. van Tooren, and W. Yao, Multidisciplinary design optimization supported by knowledge based engineering. John Wiley & Sons, (2015).

[3] A. Hosseinpour, Integration of Axiomatic Design with Quality Function Deployment for Sustainable Modular Design, M.S Thesis, Department of Mechanical Engineering University of Manitoba, (2013).

[4] Nam.P.Suh, “Complexity in Engineering,” CIRP. - Manuf. Technol., 54(2) (2005) 46-63.

[5] A. Molina-Cristobal, M. Guenov, and A. Riaz, “Enabling Exploration in the Conceptual Design and Optimisation of Complex Systems,” J. Eng. Des., (2012).

[6] G. La Rocca, “Knowledge based engineering to support aircraft design and optimization,” (2011).

[7] G. La Rocca and M. Van Tooren, “Enabling distributed multi-disciplinary design of complex products: a knowledge based engineering approach,” J Des. Res., (2007).

[8] D. P. Raymer, “Enhancing aircraft conceptual design using multidisciplinary optimization (Doctoral dissertation, Institutionen för flygteknik).,” (2002).

[9] G. La Rocca and  van T. M.J.L., “Enabling distributed multidisciplinary design of complex products: a knowledge based engineering approach,” J. Des. Res., 5(3) (2007) 333–353.

[10] M. Fioriti, L. Boggero, P. S. Prakasha, A. Mirzoyan, B. Aigner, and K. Anisimov, “Multidisciplinary aircraft integration within a collaborative and distributed design framework using the AGILE paradigm,” Prog. Aerosp. Sci., 119 (2020) 100648.

[11] I. van Gent, B. Aigner, B. Beijer, J. Jepsen, and G. La Rocca, “Knowledge architecture supporting the next generation of MDO in the AGILE paradigm,” Prog. Aerosp. Sci., 119 (2022) 100642.

[12] A. Papageorgiou, M. Tarkian, K. Amadori, and J. Ölvander, “Multidisciplinary design optimization of aerial vehicles: A review of recent advancements,” Int. J. Aerosp. Eng., 2018 (2018).

[13] J. R. R. A. Martins and A. B. Lambe, “Multidisciplinary design optimization: a survey of architectures,” AIAA J., 51(9) (2013) 2075-2013.

[14] K. Hölttä, E. S. Suh, and O. de Weck, “Tradeoff between Modularity and performance for engineered systems and products,” in Proceedings ICED 05, the 15th International Conference on Engineering Design, Melbourne, Australia, (2005), 449–450.

[15] M. Ebrahimi, J. Jeddi, and J. Roshanian, Multidisciplinary Design Optimization, 1st ed. K.N.Toosi University Press, (2019).

[16] W. Ganglin, “Key Parameters and Conceptual Configuration of Unmanned Combat Aerial Vehicle Concept,” Chinese J. Aeronaut., 22 (2009) 393-400.

[17] E. Sepulveda, H. Smith, and D. Sziroczak, “Multidisciplinary analysis of subsonic stealth unmanned combat aerial vehicles,” CEAS Aeronaut. J., 18 (2018).

[18] T. J. M. Hendrich, “Multidisciplinary Design Optimization in the Conceptual Design Phase Creating a Conceptual Design of the Blended Wing-Body with the BLISS Optimization Strategy,” Delft University of Technology, (2011).

[19] E. J. Schut, “Conceptual Design Automation: Abstraction complexity reduction by feasilisation and knowledge engineering,” (2010).

[20] D. P. Raymer, Aircraft Design: A Conceptual Approach. American Institute of Aeronautics and Astronautics(AIAA), (1992).

[21] D. Schrage, T. Beltracchi, L. Berke, A. Dodd, L. Niedling, and J. Sobieszczanski-Sobieski, “AIAA technical committee on multidisciplinary design optimization (MDO) white paper on current state of the art,” online Multidiscip. Des. Optim. Tech. Comm. Website], URL http//endo. sandia. gov/AIAA_MDOTC/sponsored/aiaa_paper. html [cited 25 Oct. 2004], (1991).

[22] Wikipedia, “Northrop Grumman X-47B,” Wikipedia, The Free Encyclopedia, (2020).

[23] Jan Roskam, Airplane design Part I. DARcorporation, (1985).

[24] C. L. Barry and E. Zimet, “UCAVs—Technological, Policy, and Operational Challenges,” Report , Center for Technology and National Security Policy National Defense University, (2001).

[25] E. Sepulveda1 and H. Smith, “Technology challenges of stealth Unmanned Combat Aerial Vehicles,” Aeronaut. J., 121 (2017) 1261-1295.

[26] H. Tianyuan and Y. Xiongqing, “Aerodynamic/Stealthy/Structural Multidisciplinary Design Optimization of Unmanned Combat Air Vehicle,” Chinese J. Aeronaut., 22 (2009) 380-386.

[27] A. De Neve and C. Wasinski, “Looking Beyond the J-UCAS Technological Demonstrator Program’s Demise,” Def. Secur. Anal., (2011) 237–249.

[28] L. R. Gilbert III, M. Omar, and A. . Farid, “An integration QFD and Axiomatic design methodology for the for satisfaction of temporary housing stakeholders.,” 8th Int. Conf. Axiomat. Des., (2014).

[29] A. M. Farid and N. P. Suh, Axiomatic Design in Large Systems. Complex Products, Buildings and Manufacturing Systems. Springer, (2016).

[30] D. D. E. Tate, “A roadmap for decomposition: activities, theories, and tools for system design (Doctoral dissertation, MIT).,” Massachusetts Institute of Technology, (1999).

[31] E. F. Knott, J. F. Shaeffer, and M. T. Tuley, Radar Cross Section, Second. SciTech, (2004).

[32] R. L. A. de Jonge, “Development of a Knowledge-Based Engineering Application to Support Conceptual Fuselage Sizing and Cabin Configuration,” Delft University of Technology, (2017).

[33] M. D. Guenov and S. G. Barker, “Application of Axiomatic Design and Design Structure Matrix to the Decomposition of Engineering Systems,” Syst. Eng., 8(1) (2004) 29–40.

[34] Q. Dong and D. E. Whitney, “Designing a requirement driven product development process,” (2001).

[35] A. A. Yassine, “An Introduction to Modeling and Analyzing Complex Product Development Processes Using the Design Structure Matrix (DSM) Method,” Urbana, 51(9) (2004) 1–17.

[36] J. Roskam, Airplane Design:Part II. Kansas: Roskam Aviation and Engineering Corporation, (1985).

[37] Northropgrumman, “www.northropgrumman.com,” (2020).