Blended wing body with boundary layer ingestion conceptual design in a multidisciplinary design analysis optimization environment

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dc.contributor.author Gao, Ziang
dc.contributor.author Smith, Howard
dc.date.accessioned 2020-02-13T11:04:45Z
dc.date.available 2020-02-13T11:04:45Z
dc.date.issued 2020-01-05
dc.identifier.citation Gao Z & Smith H. Blended wing body with boundary layer ingestion conceptual design in a multidisciplinary design analysis optimization environment. In: 2020 AIAA SciTech Forum, Orlando, Florida, 6-10 January 2020, paper number AIAA 2020-1955 en_UK
dc.identifier.isbn 978-1-62410-595-1
dc.identifier.uri https://doi.org/10.2514/6.2020-1955
dc.identifier.uri http://dspace.lib.cranfield.ac.uk/handle/1826/15128
dc.description.abstract This paper introduces the GENUS multidisciplinary concept level aircraft design and analysis environment developed by Cranfield University in recent years and it has been applied to the conceptual design of blended wing body (BWB) aircraft. Analytical disciplines include a variety of low-to-medium fidelity, physics-based and empirical methods, and aerodynamic analysis of high-order panel method. Boundary layer ingestion (BLI), as a special module, has been incorporated into the aerodynamic and propulsion analysis. The results of the Cranfield BW-11 are presented. In the highly-constrained design space, a type of highly fuel- efficient BWB concept can be studied, and the advantages of the BLI concept can also be explored based on this framework. en_UK
dc.language.iso en en_UK
dc.publisher AIAA en_UK
dc.rights Attribution-NonCommercial 4.0 International *
dc.rights.uri http://creativecommons.org/licenses/by-nc/4.0/ *
dc.subject Aircraft Design en_UK
dc.title Blended wing body with boundary layer ingestion conceptual design in a multidisciplinary design analysis optimization environment en_UK
dc.type Conference paper en_UK


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