Computational Fluid Dynamics Study on the Aerodynamics of a Blended Wing Body with Ground Effect in Subsonic Conditions
Blended Wing Body (BWB) aircraft designs have garnered significant interest due to their potential for improved aerodynamic efficiency, particularly during critical phases of flight such as landing and take-off. This study was conducted to analyse the aerodynamic performance of BWB aircraft during g...
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Isfahan University of Technology
2025-07-01
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| Series: | Journal of Applied Fluid Mechanics |
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| Online Access: | https://www.jafmonline.net/article_2713_c941aa9963d11eef1716279a0a347386.pdf |
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| author | S. Mohan P. Kumar |
| author_facet | S. Mohan P. Kumar |
| author_sort | S. Mohan |
| collection | DOAJ |
| description | Blended Wing Body (BWB) aircraft designs have garnered significant interest due to their potential for improved aerodynamic efficiency, particularly during critical phases of flight such as landing and take-off. This study was conducted to analyse the aerodynamic performance of BWB aircraft during ground effect interactions, which are crucial for understanding performance in these phases. Numerical simulations have been performed at a free-stream velocity of 18m/s. A moving ground velocity of 18 m/s has been imparted to avoid the formation of the boundary layer on the ground. Simulations were conducted at a Reynolds number of 85,525 based on MAC, with angles of attack ranging from -10 to 30 degrees and ground heights normalized by wingspan (h/b) between 0.2 and 1. The effect of the angle of attack and ground heights has been investigated. The investigations aim to capture the complex flow behaviour due to the varying ground proximities. The results at extremely close proximity revealed noticeable disparities in the normalised velocity and pressure distributions in the leeward location, highlighting the significant impact of the ground effect on aerodynamic performance. These findings contribute to a comprehensive understanding and analysis of BWB aircraft behaviour during ground proximity operations, providing insights for optimising proximities and improving safety and efficiency during landing and take-off. |
| format | Article |
| id | doaj-art-df7540bc17c846638c9277f83bf573b1 |
| institution | Matheson Library |
| issn | 1735-3572 1735-3645 |
| language | English |
| publishDate | 2025-07-01 |
| publisher | Isfahan University of Technology |
| record_format | Article |
| series | Journal of Applied Fluid Mechanics |
| spelling | doaj-art-df7540bc17c846638c9277f83bf573b12025-07-26T05:48:51ZengIsfahan University of TechnologyJournal of Applied Fluid Mechanics1735-35721735-36452025-07-011892332234810.47176/jafm.18.9.33282713Computational Fluid Dynamics Study on the Aerodynamics of a Blended Wing Body with Ground Effect in Subsonic ConditionsS. Mohan0P. Kumar1Department of Space Engineering and Rocketry, Mesra, Ranchi, 813210, Jharkhand, IndiaDepartment of Space Engineering and Rocketry, Mesra, Ranchi, 813210, Jharkhand, IndiaBlended Wing Body (BWB) aircraft designs have garnered significant interest due to their potential for improved aerodynamic efficiency, particularly during critical phases of flight such as landing and take-off. This study was conducted to analyse the aerodynamic performance of BWB aircraft during ground effect interactions, which are crucial for understanding performance in these phases. Numerical simulations have been performed at a free-stream velocity of 18m/s. A moving ground velocity of 18 m/s has been imparted to avoid the formation of the boundary layer on the ground. Simulations were conducted at a Reynolds number of 85,525 based on MAC, with angles of attack ranging from -10 to 30 degrees and ground heights normalized by wingspan (h/b) between 0.2 and 1. The effect of the angle of attack and ground heights has been investigated. The investigations aim to capture the complex flow behaviour due to the varying ground proximities. The results at extremely close proximity revealed noticeable disparities in the normalised velocity and pressure distributions in the leeward location, highlighting the significant impact of the ground effect on aerodynamic performance. These findings contribute to a comprehensive understanding and analysis of BWB aircraft behaviour during ground proximity operations, providing insights for optimising proximities and improving safety and efficiency during landing and take-off.https://www.jafmonline.net/article_2713_c941aa9963d11eef1716279a0a347386.pdfground effectpitchingpressure distributionblended wing bodyliftdrag |
| spellingShingle | S. Mohan P. Kumar Computational Fluid Dynamics Study on the Aerodynamics of a Blended Wing Body with Ground Effect in Subsonic Conditions Journal of Applied Fluid Mechanics ground effect pitching pressure distribution blended wing body lift drag |
| title | Computational Fluid Dynamics Study on the Aerodynamics of a Blended Wing Body with Ground Effect in Subsonic Conditions |
| title_full | Computational Fluid Dynamics Study on the Aerodynamics of a Blended Wing Body with Ground Effect in Subsonic Conditions |
| title_fullStr | Computational Fluid Dynamics Study on the Aerodynamics of a Blended Wing Body with Ground Effect in Subsonic Conditions |
| title_full_unstemmed | Computational Fluid Dynamics Study on the Aerodynamics of a Blended Wing Body with Ground Effect in Subsonic Conditions |
| title_short | Computational Fluid Dynamics Study on the Aerodynamics of a Blended Wing Body with Ground Effect in Subsonic Conditions |
| title_sort | computational fluid dynamics study on the aerodynamics of a blended wing body with ground effect in subsonic conditions |
| topic | ground effect pitching pressure distribution blended wing body lift drag |
| url | https://www.jafmonline.net/article_2713_c941aa9963d11eef1716279a0a347386.pdf |
| work_keys_str_mv | AT smohan computationalfluiddynamicsstudyontheaerodynamicsofablendedwingbodywithgroundeffectinsubsonicconditions AT pkumar computationalfluiddynamicsstudyontheaerodynamicsofablendedwingbodywithgroundeffectinsubsonicconditions |