References
[1]. Moore M, “X-29 Forward Swept Wing Aerodynamic Overview.” In Applied Aerodynamics Conference. Danvers, MA,U. S. A. : American Institute of Aeronautics and Astronautics, 1983.
[2]. Risse, K, Anton, E, Lammering, T, Franz, K, Hoernschemeyer, R. (2012). An Integrated Environment for Preliminary Aircraft Design and Optimization. 53rd AIAA/ASME/ASCE/ AHS/ASC Structures, Structural Dynamics and Materials Conference, Honolulu, Hawaii.
[3]. Risse, K, (2016) “Preliminary Overall Aircraft Design with Hybrid Laminar Flow Control”, Ph. D. dissertation, RWTH Aachen University, see also: Shaker, Aachen, Dec. 2016.
[4]. Chiozzotto, G. P. (2017). Initial Weight Estimate of Advanced Transport Aircraft Concepts Considering Aeroelastic Effects. 55th AIAA Aerospace Sciences Meeting, Texas, USA.
[5]. Kruse, M, Wunderlich, T, Heinrich, L. (2012) A Conceptual Study of a Transonic NLF Transport Aircraft with Forward Swept Wings. 30th AIAA Applied Aerodynamics Conference, New Orleans, USA.
[6]. Seitz A, Hübner A, Risse K. (2019) The DLR TuLam project: design of a short and medium range transport aircraft with forward swept NLF wing, CEAS Aeronautical Journal, pp. 111.
[7]. Tremolet, A, Gauvrit-Ledogar, J, Brevault, L, Defoort S, Morel, F, (2019), Multidisciplinary Overall Aircraft Design and Optimisation of Blended Wing Body Configurations, 1 - 4 July 2019, Madrid, Spain.
[8]. Sgueglia, A, Schmollgruber, P, Bartoli, N, Atinault, O, Benard, E, Morlier, J. (2018) . Exploration and Sizing of a Large Passenger Aircraft with Distributed Ducted Electric Fans. 2018 AIAA Aerospace Sciences Meeting, Kissimmee, USA.
[9]. Neal D A, Good M G, Johnston C O, Robertshaw H H, Mason W H and Inman D J 2004 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Material Conf. p 1727.
[10]. Secanell M, Suleman A. Gamboa P 2005 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conf. p 1891.
[11]. Chen Q, Bai P, Ying WL, Leng JS, Liu ZQ 2010 Acta Aerodynamica Sinica vol 28 p 46.
[12]. Swaim RL, Newman BA 1985 Journal of Guidance Control & Dynamics vol 9 p 352.
[13]. Northrop Grumman Corporation 1999 Aircraft with variable forward-swept wing USA, US5984231.
[14]. Yoshimoto, M, and Uchiyama. N, “Optimization of Canard Surface Positioning of Supersonic Business Jet for Low Boom and Low Drag Design,” AIAA Paper 2003-3576, January 2012.
[15]. Ueno, A, and Makino, Y, “Low-Boom and Low-Drag Design of Small Supersonic Transport Considering Propulsion Airframe Integration,” JAXA-RM-18-001E, 2018.
[16]. Sriram K. Rallabhandi, Wu, L, and Karl, G, “Boom-Constrained Drag Minimization for Design of Supersonic Concepts,” 48th AIAA Aerospace Sciences Meeting and Exhibit, Aerospace Sciences Meetings, AIAA-2010-844.
[17]. Horinouchi, S, “Conceptual Design of a Low Boom SSBJ,” 43rd AIAA Aerospace Sciences Meeting and Exhibit, Aerospace Sciences Meetings, AIAA-2005-1018, 2005.
[18]. Kishi, Y, Kanazaki, M, and Makino, Y, “Numerical Investigation of Sonic Boom Strength for Forward-Swept Wing Based on Euler Equation and Augmented Burgers Equation”, 48th Fluid Dynamics Conference/36th Aerospace Numerical Simulation Symposium, 2018 (in Japanese).
Cite this article
Li,J. (2023). Aerodynamics-based forward-swept wing structure optimization. Applied and Computational Engineering,10,297-306.
Data availability
The datasets used and/or analyzed during the current study will be available from the authors upon reasonable request.
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References
[1]. Moore M, “X-29 Forward Swept Wing Aerodynamic Overview.” In Applied Aerodynamics Conference. Danvers, MA,U. S. A. : American Institute of Aeronautics and Astronautics, 1983.
[2]. Risse, K, Anton, E, Lammering, T, Franz, K, Hoernschemeyer, R. (2012). An Integrated Environment for Preliminary Aircraft Design and Optimization. 53rd AIAA/ASME/ASCE/ AHS/ASC Structures, Structural Dynamics and Materials Conference, Honolulu, Hawaii.
[3]. Risse, K, (2016) “Preliminary Overall Aircraft Design with Hybrid Laminar Flow Control”, Ph. D. dissertation, RWTH Aachen University, see also: Shaker, Aachen, Dec. 2016.
[4]. Chiozzotto, G. P. (2017). Initial Weight Estimate of Advanced Transport Aircraft Concepts Considering Aeroelastic Effects. 55th AIAA Aerospace Sciences Meeting, Texas, USA.
[5]. Kruse, M, Wunderlich, T, Heinrich, L. (2012) A Conceptual Study of a Transonic NLF Transport Aircraft with Forward Swept Wings. 30th AIAA Applied Aerodynamics Conference, New Orleans, USA.
[6]. Seitz A, Hübner A, Risse K. (2019) The DLR TuLam project: design of a short and medium range transport aircraft with forward swept NLF wing, CEAS Aeronautical Journal, pp. 111.
[7]. Tremolet, A, Gauvrit-Ledogar, J, Brevault, L, Defoort S, Morel, F, (2019), Multidisciplinary Overall Aircraft Design and Optimisation of Blended Wing Body Configurations, 1 - 4 July 2019, Madrid, Spain.
[8]. Sgueglia, A, Schmollgruber, P, Bartoli, N, Atinault, O, Benard, E, Morlier, J. (2018) . Exploration and Sizing of a Large Passenger Aircraft with Distributed Ducted Electric Fans. 2018 AIAA Aerospace Sciences Meeting, Kissimmee, USA.
[9]. Neal D A, Good M G, Johnston C O, Robertshaw H H, Mason W H and Inman D J 2004 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Material Conf. p 1727.
[10]. Secanell M, Suleman A. Gamboa P 2005 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conf. p 1891.
[11]. Chen Q, Bai P, Ying WL, Leng JS, Liu ZQ 2010 Acta Aerodynamica Sinica vol 28 p 46.
[12]. Swaim RL, Newman BA 1985 Journal of Guidance Control & Dynamics vol 9 p 352.
[13]. Northrop Grumman Corporation 1999 Aircraft with variable forward-swept wing USA, US5984231.
[14]. Yoshimoto, M, and Uchiyama. N, “Optimization of Canard Surface Positioning of Supersonic Business Jet for Low Boom and Low Drag Design,” AIAA Paper 2003-3576, January 2012.
[15]. Ueno, A, and Makino, Y, “Low-Boom and Low-Drag Design of Small Supersonic Transport Considering Propulsion Airframe Integration,” JAXA-RM-18-001E, 2018.
[16]. Sriram K. Rallabhandi, Wu, L, and Karl, G, “Boom-Constrained Drag Minimization for Design of Supersonic Concepts,” 48th AIAA Aerospace Sciences Meeting and Exhibit, Aerospace Sciences Meetings, AIAA-2010-844.
[17]. Horinouchi, S, “Conceptual Design of a Low Boom SSBJ,” 43rd AIAA Aerospace Sciences Meeting and Exhibit, Aerospace Sciences Meetings, AIAA-2005-1018, 2005.
[18]. Kishi, Y, Kanazaki, M, and Makino, Y, “Numerical Investigation of Sonic Boom Strength for Forward-Swept Wing Based on Euler Equation and Augmented Burgers Equation”, 48th Fluid Dynamics Conference/36th Aerospace Numerical Simulation Symposium, 2018 (in Japanese).