Relevant bibliographies by topics / Blended-wing-body aircraft

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Academic literature on the topic 'Blended-wing-body aircraft'

Author: Grafiati
Published: 4 June 2021
Last updated: 19 February 2022

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Journal articles on the topic "Blended-wing-body aircraft"

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Qin, N., A. Vavalle, A. Le Moigne, M. Laban, K. Hackett, and P. Weinerfelt. "Aerodynamic considerations of blended wing body aircraft." Progress in Aerospace Sciences 40, no. 6 (August 2004): 321–43. http://dx.doi.org/10.1016/j.paerosci.2004.08.001.

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Qin, Ning, Armando Vavalle, and Alan Le Moigne. "Spanwise Lift Distribution for Blended Wing Body Aircraft." Journal of Aircraft 42, no. 2 (March 2005): 356–65. http://dx.doi.org/10.2514/1.4229.

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Zhu, Wensheng, Xiongqing Yu, and Yu Wang. "Layout Optimization for Blended Wing Body Aircraft Structure." International Journal of Aeronautical and Space Sciences 20, no. 4 (May 16, 2019): 879–90. http://dx.doi.org/10.1007/s42405-019-00172-7.

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Dimopoulos, Thomas, Pericles Panagiotou, and Kyros Yakinthos. "Stability study and flight simulation of a blended-wing-body UAV." MATEC Web of Conferences 304 (2019): 02013. http://dx.doi.org/10.1051/matecconf/201930402013.

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This article is a product of the design process of a Blended-Wing- Body Unmanned Aerial Vehicle (BWB UAV). The BWB geometry blends the wing and the fuselage so that the fuselage also contributes in lift generation. This geometry reduces the lift to drag ratio significantly, however it also compromises the aircraft’s stability and controllability, since there is no horizontal and vertical tail. As these features are absent from the BWB layout, the need to incorporate their functions in the new geometry arises so that they cover stability demands sufficiently, according to aircraft of similar si
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Velicki, A., and P. Thrash. "Blended wing body structural concept development." Aeronautical Journal 114, no. 1158 (August 2010): 513–19. http://dx.doi.org/10.1017/s0001924000004000.

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Abstract A lightweight robust airframe design is one of the key technological advancements necessary for the successful launch of a blended wing body aircraft. The non-circular pressure cabin dictates that substantial improvements beyond current state-of-the-art aluminium and composite structures is needed, and that improvements of this magnitude will require radically new airframe design and manufacturing practices. Such an approach is described in this paper. It is a highly integrated structural concept that is tailored and optimised to fully exploit the orthotropic nature and unique process
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Xu, Xin, Qiang Li, Dawei Liu, Keming Cheng, and Dehua Chen. "Geometric Effects Analysis and Verification of V-Shaped Support Interference on Blended Wing Body Aircraft." Applied Sciences 10, no. 5 (February 28, 2020): 1596. http://dx.doi.org/10.3390/app10051596.

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A special V-shaped support for blended wing body aircraft was designed and applied in high-speed wind tunnel tests. In order to reduce the support interference and explore the design criteria of the V-shaped support, interference characteristics and geometric parameter effects of V-shaped support on blended wing body aircraft were numerically studied. According to the numerical results, the corresponding dummy V-shaped supports were designed and manufactured, and verification tests was conducted in a 2.4 m × 2.4 m transonic wind tunnel. The test results were in good agreement with the numerica
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Romli, Fairuz Izzuddin, and Mohd Syahidie Kamaruddin. "Emissions Performance Study for Conventional Aircraft Designs." Applied Mechanics and Materials 225 (November 2012): 385–90. http://dx.doi.org/10.4028/www.scientific.net/amm.225.385.

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Conventional aircraft designs have been highly successful within commercial passengers transport markets for a very long time, as evident from current fleet of many airlines. However, with the anticipated stricter environmental regulations to be imposed on future flight operations by the related governing bodies, the relevance of conventional aircraft designs to remain competitive has been questioned. On the other hand, some research ventures have been made to pursue revolutionary designs like blended wing body (BWB). This study aims to preliminarily assess the comparison of expected future em
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van Dommelen, Jorrit, and Roelof Vos. "Conceptual design and analysis of blended-wing-body aircraft." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 228, no. 13 (January 29, 2014): 2452–74. http://dx.doi.org/10.1177/0954410013518696.

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Due to the unconventional nature of the blended wing body (BWB) no off-the-shelf software package exists for its conceptual design. This study details a first step towards the implementation of traditional and BWB-specific design and analysis methods into a software tool to enable preliminary sizing of a BWB. The tool is able to generate and analyze different BWB configurations on a conceptual level. This paper investigates three different BWB configurations. The first configuration is an aft-swept BWB with aft-mounted engines, the second configuration is an aft-swept BWB with wing-mounted eng
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Hong, Wei Jiang, and Dong Li Ma. "Influence of Control Coupling Effect on Landing Performance of Flying Wing Aircraft." Applied Mechanics and Materials 829 (March 2016): 110–17. http://dx.doi.org/10.4028/www.scientific.net/amm.829.110.

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As flying wing aircraft has no tail and adopts blended-wing-body design, most of flying wing aircrafts are directional unstable. Pitching moment couples seriously with rolling and yawing moment when control surfaces are deflected, bringing insecurity to landing stage. Numerical simulation method and semi-empirical equation estimate method were combined to obtain a high aspect ratio flying wing aircraft’s aerodynamic coefficients. Modeling and simulation of landing stage were established by MATLAB/Simulink. The control coupling effect on lift and drag characteristics and anti-crosswind landing
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Mulyanto, Taufiq, and M. Luthfi Nurhakim. "CONCEPTUAL DESIGN OF BLENDED WING BODY BUSINESS JET AIRCRAFT." Journal of KONES. Powertrain and Transport 20, no. 4 (January 1, 2015): 299–306. http://dx.doi.org/10.5604/12314005.1137630.

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Dissertations / Theses on the topic "Blended-wing-body aircraft"

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Okonkwo, Paulinus Peter Chukwuemeka. "Conceptual design methodology for blended wing body aircraft." Thesis, Cranfield University, 2016. http://dspace.lib.cranfield.ac.uk/handle/1826/10132.

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The desire to create an environmentally friendly aircraft that is aerodynamically efficient and capable of conveying large number of passengers over long ranges at reduced direct operating cost led aircraft designers to develop the Blended Wing Body(BWB) aircraft concept. The BWB aircraft represents a paradigm shift in the design of aircraft. The design offers immense aerodynamics and environmental benefits and is suitable for the integration of advanced systems and concepts like laminar flow technology, jet flaps and distributed propulsion. However, despite these benefits, the BWB is yet to b
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Ikeda, Toshihiro, and toshi ikeda@gmail com. "Aerodynamic Analysis of a Blended-Wing-Body Aircraft Configuration." RMIT University. Aerospace, Mechanical and Manufacturing Engineering, 2006. http://adt.lib.rmit.edu.au/adt/public/adt-VIT20070122.163030.

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In recent years unconventional aircraft configurations, such as Blended-Wing-Body (BWB) aircraft, are being investigated and researched with the aim to develop more efficient aircraft configurations, in particular for very large transport aircraft that are more efficient and environmentally-friendly. The BWB configuration designates an alternative aircraft configuration where the wing and fuselage are integrated which results essentially in a hybrid flying wing shape. The first example of a BWB design was researched at the Loughead Company in the United States of America in 1917. T
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Vavalle, Armando. "Response surface aerodynamic optimisation for blended wing body aircraft." Thesis, Cranfield University, 2005. http://dspace.lib.cranfield.ac.uk/handle/1826/11015.

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This study is concerned with a methodology for the aerodynamic analysis and preliminary design of a novel configuration for high subsonic civil transport, based on the flying wing concept, known a Blended Wing Body (BWB). A response surface based optimisation method is developed, enabling the designer to monitor the effect of shape modification on the controllability of the aircraft in both longitudinal and lateral/directional motion and on the Wing structural weight, while maximising the aerodynamic efficiency. The design aspects considered included high- speed aerodynamics, flight static-sta
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Ur, Rahman Naveed. "Propulsion and flight controls integration for the blended wing body aircraft." Thesis, Cranfield University, 2009. http://hdl.handle.net/1826/4095.

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The Blended Wing Body (BWB) aircraft offers a number of aerodynamic perfor- mance advantages when compared with conventional configurations. However, while operating at low airspeeds with nominal static margins, the controls on the BWB aircraft begin to saturate and the dynamic performance gets sluggish. Augmenta- tion of aerodynamic controls with the propulsion system is therefore considered in this research. Two aspects were of interest, namely thrust vectoring (TVC) and flap blowing. An aerodynamic model for the BWB aircraft with blown flap effects was formulated using empirical and vortex
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Kays, Cory Asher. "Multidisciplinary methods for performing trade studies on blended wing body aircraft." Thesis, Massachusetts Institute of Technology, 2013. http://hdl.handle.net/1721.1/82485.

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Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2013.<br>This electronic version was submitted and approved by the author's academic department as part of an electronic thesis pilot project. The certified thesis is available in the Institute Archives and Special Collections.<br>Cataloged from department-submitted PDF version of thesis<br>Includes bibliographical references (p. 99-102).<br>Multidisciplinary design optimization (MDO) is becoming an essential tool for the design of engineering systems due to the inherent coupling between discipline an
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Dippold, Vance Fredrick III. "Numerical Assessment of the Performance of Jet-Wing Distributed Propulsion on Blended-Wing-Body Aircraft." Thesis, Virginia Tech, 2003. http://hdl.handle.net/10919/34878.

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<p> Conventional airliners use two to four engines in a Cayley-type arrangement to provide thrust, and the thrust from these engines is typically concentrated right behind the engine. Distributed propulsion is the idea of redistributing the thrust across most, or all, of the wingspan of an aircraft. This can be accomplished by using several large engines and using a duct to spread out the exhaust flow to form a jet-wing or by using many small engines spaced along the span of the wing. Jet-wing distributed propulsion was originally suggested by Kuchemann as a way to improve propulsive effici
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Ko, Yan-Yee Andy. "The Multidisciplinary Design Optimization of a Distributed Propulsion Blended-Wing-Body Aircraft." Diss., Virginia Tech, 2003. http://hdl.handle.net/10919/27257.

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The purpose of this study is to examine the multidisciplinary design optimization (MDO) of a distributed propulsion blended-wing-body (BWB) aircraft. The BWB is a hybrid shape resembling a flying wing, placing the payload in the inboard sections of the wing. The distributed propulsion concept involves replacing a small number of large engines with many smaller engines. The distributed propulsion concept considered here ducts part of the engine exhaust to exit out along the trailing edge of the wing. The distributed propulsion concept affects almost every aspect of the BWB design. Methods to m
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van, Wyk David. "Guidance, navigation and control of a small, unmanned blended wing body aircraft." Master's thesis, Faculty of Engineering and the Built Environment, 2020. http://hdl.handle.net/11427/32426.

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The purpose of this research is to document the design and optimisation of a full suite of guidance, navigation and control (GNC) algorithms for a small unmanned aerial vehicle (UAV), the Skywalker X8. This was performed so as to fill a void in the available literature on the selected airframe, which currently only focuses on aspects such as aerodynamic modelling, advanced controller design, or uses of the airframe to perform higher level tasks. All of these research areas make use of off-the-shelf flight controllers, but these are not always the most appropriate foundations for more advanced
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de, Castro Helena V. "Flying and handling qualities of a fly-by-wire blended-wing-body civil transport aircraft." Thesis, Cranfield University, 2003. http://hdl.handle.net/1826/119.

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The blended-wing-body (BWB) configuration appears as a promising contender for the next generation of large transport aircraft. The idea of blending the wing with the fuselage and eliminating the tail is not new, it has long been known that tailless aircraft can suffer from stability and control problems that must be addressed early in the design. This thesis is concerned with identifying and then evaluating the flight dynamics, stability, flight controls and handling qualities of a generic BWB large transport aircraft concept. Longitudinal and lateral-directional static and dynamic stability
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Hanlon, Christopher J. (Christopher Joseph) 1978. "Engine design implications for a blended wing-body aircraft with boundary later ingestion." Thesis, Massachusetts Institute of Technology, 2003. http://hdl.handle.net/1721.1/82759.

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Books on the topic "Blended-wing-body aircraft"

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Kozek, Martin, and Alexander Schirrer, eds. Modeling and Control for a Blended Wing Body Aircraft. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-10792-9.

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Kozek, Martin, and Alexander Schirrer. Modeling and Control for a Blended Wing Body Aircraft: A Case Study. Springer, 2016.

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Hallion, Richard, and Bruce Larrimer. Beyond Tube-And-Wing: The X-48 Blended Wing-Body and NASA's Quest to Reshape Future Transport Aircraft. National Aeronautics and Space Administration, 2020.

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Book chapters on the topic "Blended-wing-body aircraft"

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Kozek, M., A. Schirrer, B. Mohr, D. Paulus, T. Salmon, M. Hornung, C. Rößler, F. Stroscher, and A. Seitz. "Overview and Motivation." In Modeling and Control for a Blended Wing Body Aircraft, 1–25. Cham: Springer International Publishing, 2014. http://dx.doi.org/10.1007/978-3-319-10792-9_1.

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Baier, H., M. Hornung, B. Mohr, D. Paulus, Ö. Petersson, C. Rößler, F. Stroscher, and T. Salmon. "Conceptual Design." In Modeling and Control for a Blended Wing Body Aircraft, 29–45. Cham: Springer International Publishing, 2014. http://dx.doi.org/10.1007/978-3-319-10792-9_2.

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Stroscher, F., A. Schirrer, M. Valášek, Z. Šika, T. Vampola, B. Paluch, D. Joly, et al. "Numerical Simulation Model." In Modeling and Control for a Blended Wing Body Aircraft, 47–104. Cham: Springer International Publishing, 2014. http://dx.doi.org/10.1007/978-3-319-10792-9_3.

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Valášek, M., Z. Šika, T. Vampola, and S. Hecker. "Reduced-Order Modeling." In Modeling and Control for a Blended Wing Body Aircraft, 105–27. Cham: Springer International Publishing, 2014. http://dx.doi.org/10.1007/978-3-319-10792-9_4.

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Westermayer, C., and A. Schirrer. "Control Goals." In Modeling and Control for a Blended Wing Body Aircraft, 131–46. Cham: Springer International Publishing, 2014. http://dx.doi.org/10.1007/978-3-319-10792-9_5.

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Schirrer, A., M. Kozek, F. Demourant, and G. Ferreres. "Feedback Control Designs." In Modeling and Control for a Blended Wing Body Aircraft, 147–226. Cham: Springer International Publishing, 2014. http://dx.doi.org/10.1007/978-3-319-10792-9_6.

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Haniš, T., M. Hromčík, A. Schirrer, M. Kozek, and C. Westermayer. "Feed-Forward Control Designs." In Modeling and Control for a Blended Wing Body Aircraft, 227–63. Cham: Springer International Publishing, 2014. http://dx.doi.org/10.1007/978-3-319-10792-9_7.

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Kozek, M., A. Schirrer, F. Stroscher, M. Valášek, Z. Šika, T. Vampola, T. Belschner, and A. Wildschek. "Validation, Discussion and Outlook." In Modeling and Control for a Blended Wing Body Aircraft, 267–95. Cham: Springer International Publishing, 2014. http://dx.doi.org/10.1007/978-3-319-10792-9_8.

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Schirrer, Alexander, Martin Kozek, and Stefan Jakubek. "Convex Design for Lateral Control of a Blended Wing Body Aircraft." In Mechanics and Model-Based Control of Advanced Engineering Systems, 255–64. Vienna: Springer Vienna, 2013. http://dx.doi.org/10.1007/978-3-7091-1571-8_28.

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Galea, E. R., L. Filippidis, Z. Wang, P. J. Lawrence, and J. Ewer. "Evacuation Analysis of 1000+ Seat Blended Wing Body Aircraft Configurations: Computer Simulations and Full-scale Evacuation Experiment." In Pedestrian and Evacuation Dynamics, 151–61. Boston, MA: Springer US, 2011. http://dx.doi.org/10.1007/978-1-4419-9725-8_14.

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Conference papers on the topic "Blended-wing-body aircraft"

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Qin, N. "Aerodynamic Studies for Blended Wing Body Aircraft." In 9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2002. http://dx.doi.org/10.2514/6.2002-5448.

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Guo, Yueping, Casey L. Burley, and Russell H. Thomas. "On Noise Assessment for Blended Wing Body Aircraft." In 52nd Aerospace Sciences Meeting. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2014. http://dx.doi.org/10.2514/6.2014-0365.

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Peigin, Sergey, and Boris Epstein. "CFD Driven Optimization of Blended Wing Body Aircraft." In 24th AIAA Applied Aerodynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2006. http://dx.doi.org/10.2514/6.2006-3457.

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Peterson, Tim, and Peter Grant. "Handling Qualities of a Blended Wing Body Aircraft." In AIAA Atmospheric Flight Mechanics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2011. http://dx.doi.org/10.2514/6.2011-6542.

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Weil Brenner, Martin, Jean-yves Trepanier, Christophe Tribes, and Eddy Petro. "Conceptual Design Framework for Blended Wing Body Aircraft." In 12th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference and 14th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2012. http://dx.doi.org/10.2514/6.2012-5649.

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Lyu, Zhoujie, and Joaquim R. R. A. Martins. "Aerodynamic Shape Optimization of a Blended-Wing-Body Aircraft." In 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2013. http://dx.doi.org/10.2514/6.2013-283.

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Guo, Yueping, Michael Czech, and Russell H. Thomas. "Open Rotor Noise Shielding by Blended-Wing-Body Aircraft." In 53rd AIAA Aerospace Sciences Meeting. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2015. http://dx.doi.org/10.2514/6.2015-1214.

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Singh, Garima, Vassili Toropov, and James Eves. "Topology Optimization of a Blended-Wing-Body Aircraft Structure." In 17th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2016. http://dx.doi.org/10.2514/6.2016-3364.

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Brown, Malcom, and Roelof Vos. "Conceptual Design and Evaluation of Blended-Wing Body Aircraft." In 2018 AIAA Aerospace Sciences Meeting. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2018. http://dx.doi.org/10.2514/6.2018-0522.

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Yi, Jian, Xin-min Dong, Yong Chen, Jian-hui Zhi, Bing-xu Zhou, and Xian-chi Huang. "Nonlinear Control Allocation for a Blended Wing Body Aircraft." In 2016 International Conference on Electrical Engineering and Automation (EEA2016). WORLD SCIENTIFIC, 2017. http://dx.doi.org/10.1142/9789813220362_0073.

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