The Effect of Gust on Blended-Wing-Body Civil Aircraft

Chen Fang Cai; Jiang Hao Wu; Bin Liang

doi:10.4028/www.scientific.net/AMR.1016.359

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HomeAdvanced Materials ResearchAdvanced Materials Research Vol. 1016The Effect of Gust on Blended-Wing-Body Civil...

The Effect of Gust on Blended-Wing-Body Civil Aircraft

Abstract:

In this paper, aerodynamic properties of Blended Wing Body (BWB) civil aircraft are studied by two models: one calls complete model that is computed by numerical simulation coupling equations of motion with the Navier-Stokes equations, and the other doesn’t consider the equations of motion (without dynamic response). The results show that the model without dynamic response can also correctly predict the trend of the dynamic properties compared with complete model. Nevertheless, there are some quantitative differences existing between the complete model and the model without dynamic response.

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Periodical:

Advanced Materials Research (Volume 1016)

Pages:

359-364

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.1016.359

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Online since:

August 2014

Authors:

Chen Fang Cai, Jiang Hao Wu*, Bin Liang

Keywords:

Aerodynamic, Blended-Wing-Body, Computational Fluid Dynamics (CFD), Dynamic Response, Gust

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* - Corresponding Author

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