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2020 | OriginalPaper | Chapter

11. Blended Wing Body Design

Authors : Julie Gauvrit-Ledogar, Arnault Tremolet, Loïc Brevault

Published in: Aerospace System Analysis and Optimization in Uncertainty

Publisher: Springer International Publishing

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Abstract

For the coming years, the commercial air transport industry will have to take up the huge challenge of both reducing the costs associated to the aircraft fuel consumption and reduce the global air transport environmental footprint. Reaching these two objectives leads to the reduction of the fuel consumption, the reduction of the pollutant emissions (specifically CO2 and NOx emissions), and the reduction of noise emissions.

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Literature
go back to reference Airbus (2014a). Airbus family figures, ed. July 2014. Airbus (2014a). Airbus family figures, ed. July 2014.
go back to reference Airbus (2014b). Airport operations. A350-1000 airport compatibility brochure, issue 1, ref. v00pr1413357. Airbus (2014b). Airport operations. A350-1000 airport compatibility brochure, issue 1, ref. v00pr1413357.
go back to reference EASA (2014). Certification Specifications and Acceptable Means of Compliance for Large Aeroplanes CS-25. EASA (2014). Certification Specifications and Acceptable Means of Compliance for Large Aeroplanes CS-25.
go back to reference EASA (2017). Type-certificate data sheet for ge90 series engines. EASA (2017). Type-certificate data sheet for ge90 series engines.
go back to reference European Commission (2011). Flightpath 2050–Europe’s vision for aviation maintaining global leadership and serving society’s needs–report of the high-level group on aviation research. European Commission (2011). Flightpath 2050–Europe’s vision for aviation maintaining global leadership and serving society’s needs–report of the high-level group on aviation research.
go back to reference Fredericks, W., Antcliff, K., Costa, G., Deshpande, N., Moore, M., San Miguel, E., and Snyder, A. (2010). Aircraft conceptual design using vehicle sketch pad. In 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Orlando, FL, USA. Fredericks, W., Antcliff, K., Costa, G., Deshpande, N., Moore, M., San Miguel, E., and Snyder, A. (2010). Aircraft conceptual design using vehicle sketch pad. In 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Orlando, FL, USA.
go back to reference Gauvrit-Ledogar, J., Defoort, S., Tremolet, A., and Morel, F. (2018). Multidisciplinary overall aircraft design process dedicated to blended wing body configurations. In 2018 Aviation Technology, Integration, and Operations Conference, Atlanta, Georgia. Gauvrit-Ledogar, J., Defoort, S., Tremolet, A., and Morel, F. (2018). Multidisciplinary overall aircraft design process dedicated to blended wing body configurations. In 2018 Aviation Technology, Integration, and Operations Conference, Atlanta, Georgia.
go back to reference Gray, J. S., Moore, K. T., and Naylor, B. A. (2010). OpenMDAO: An open-source framework for multidisciplinary analysis and optimization. In 13th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Fort Worth, TX, USA. Gray, J. S., Moore, K. T., and Naylor, B. A. (2010). OpenMDAO: An open-source framework for multidisciplinary analysis and optimization. In 13th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Fort Worth, TX, USA.
go back to reference Greitzer, E., Bonnefoy, P., De la Rosa Blanco, E., Dorbian, C., Drela, M., Hall, D., Hansman, R., Hileman, J., Liebeck, R., Lovegren, J., et al. (2010). N+ 3 aircraft concept designs and trade studies. volume 2; appendices-design methodologies for aerodynamics, structures, weight, and thermodynamic cycles. NASA/CR-2010-216794/VOL2, E-17419-2. Greitzer, E., Bonnefoy, P., De la Rosa Blanco, E., Dorbian, C., Drela, M., Hall, D., Hansman, R., Hileman, J., Liebeck, R., Lovegren, J., et al. (2010). N+ 3 aircraft concept designs and trade studies. volume 2; appendices-design methodologies for aerodynamics, structures, weight, and thermodynamic cycles. NASA/CR-2010-216794/VOL2, E-17419-2.
go back to reference Gur, O., Mason, W. H., and Schetz, J. A. (2010). Full-configuration drag estimation. Journal of Aircraft, 47(4):1356–1367.CrossRef Gur, O., Mason, W. H., and Schetz, J. A. (2010). Full-configuration drag estimation. Journal of Aircraft, 47(4):1356–1367.CrossRef
go back to reference Haftmann, B., Debbeler, F.-J., and Gielen, H. (1988). Takeoff drag prediction for airbus a300-600 and a310 compared with flight test results. Journal of Aircraft, 25(12):1088–1096.CrossRef Haftmann, B., Debbeler, F.-J., and Gielen, H. (1988). Takeoff drag prediction for airbus a300-600 and a310 compared with flight test results. Journal of Aircraft, 25(12):1088–1096.CrossRef
go back to reference Holder, W. G. (1998). Northrop Grumman B-2 Spirit: An Illustrated History. Schiffer Pub. Holder, W. G. (1998). Northrop Grumman B-2 Spirit: An Illustrated History. Schiffer Pub.
go back to reference Ko, Y.-Y. A. (2003). The multidisciplinary design optimization of a distributed propulsion blended-wing-body aircraft. PhD thesis, Virginia Tech. Ko, Y.-Y. A. (2003). The multidisciplinary design optimization of a distributed propulsion blended-wing-body aircraft. PhD thesis, Virginia Tech.
go back to reference Lambe, A. and Martins, J. (2011). A unified description of MDO architectures. In 9th World Congress on Structural and Multidisciplinary Optimization, Shizuoka, Japan. Lambe, A. and Martins, J. (2011). A unified description of MDO architectures. In 9th World Congress on Structural and Multidisciplinary Optimization, Shizuoka, Japan.
go back to reference Liebeck, R. H. (2004). Design of the blended wing body subsonic transport. Journal of aircraft, 41(1):10–25.CrossRef Liebeck, R. H. (2004). Design of the blended wing body subsonic transport. Journal of aircraft, 41(1):10–25.CrossRef
go back to reference Lowry, J. G. and Polhamus, E. C. (1957). A method for predicting lift increments due to flap deflection at low angles of attack in incompressible flow. NACA Technical Note 3911. Lowry, J. G. and Polhamus, E. C. (1957). A method for predicting lift increments due to flap deflection at low angles of attack in incompressible flow. NACA Technical Note 3911.
go back to reference Nickol, C. (2012). Hybrid wing body configuration scaling study. In 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Nashville, TN, USA. Nickol, C. (2012). Hybrid wing body configuration scaling study. In 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Nashville, TN, USA.
go back to reference Niţă, M. and Scholz, D. (2012). Estimating the Oswald factor from basic aircraft geometrical parameters. German Aerospace Congress, Berlin, Germany. Niţă, M. and Scholz, D. (2012). Estimating the Oswald factor from basic aircraft geometrical parameters. German Aerospace Congress, Berlin, Germany.
go back to reference Nită, M. F. (2012). Contributions to Aircraft Preliminary Design and Optimization. Ph. D. Thesis, Politehnica University of Bucharest, Bucharest, Romania. Nită, M. F. (2012). Contributions to Aircraft Preliminary Design and Optimization. Ph. D. Thesis, Politehnica University of Bucharest, Bucharest, Romania.
go back to reference Raymer, D. (2012). Aircraft Design: A Conceptual Approach 5e and RDSWin STUDENT. American Institute of Aeronautics and Astronautics, Inc.CrossRef Raymer, D. (2012). Aircraft Design: A Conceptual Approach 5e and RDSWin STUDENT. American Institute of Aeronautics and Astronautics, Inc.CrossRef
go back to reference Torenbeek, E. (2013). Advanced aircraft design: conceptual design, analysis and optimization of subsonic civil airplanes. John Wiley & Sons.CrossRef Torenbeek, E. (2013). Advanced aircraft design: conceptual design, analysis and optimization of subsonic civil airplanes. John Wiley & Sons.CrossRef
go back to reference Yang, S., Page, M., and Smetak, E. (2018). Achievement of NASA new aviation horizons n+2 goals with a blended-wing-body x-plane designed for the regional jet and single-aisle jet markets. In 2018 AIAA Aerospace Sciences Meeting, AIAA SciTech Forum, Kissimmee, FL, USA. Yang, S., Page, M., and Smetak, E. (2018). Achievement of NASA new aviation horizons n+2 goals with a blended-wing-body x-plane designed for the regional jet and single-aisle jet markets. In 2018 AIAA Aerospace Sciences Meeting, AIAA SciTech Forum, Kissimmee, FL, USA.
Metadata
Title
Blended Wing Body Design
Authors
Julie Gauvrit-Ledogar
Arnault Tremolet
Loïc Brevault
Copyright Year
2020
DOI
https://doi.org/10.1007/978-3-030-39126-3_11