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eISSN: 2581-9615 || CODEN: WJARAI || Impact Factor 8.2 ||  CrossRef DOI

Research and review articles are invited for publication in April 2026 (Volume 30, Issue 1) Submit manuscript

Research on stability for blended-wing-body aircraft

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  • Research on stability for blended-wing-body aircraft

Lucky Bose 1, *, Isfaq Ahmed Rafsun 2 and Junquan Fu 1

1 School of Aircraft Engineering, Nanchang Hangkong University, Aeroengine.
2 School of Aeronautics, Nanjing University of Aeronautics and Astronautics, Aeroengine.
 
Research Article
World Journal of Advanced Research and Reviews, 2024, 23(03), 2919-2932
Article DOI: 10.30574/wjarr.2024.23.3.2961
DOI url: https://doi.org/10.30574/wjarr.2024.23.3.2961
 
Received on 16 August 2024; revised on 25 September 2024; accepted on 27 September 2024
 
The primary goal of this research is to research the stability properties of a blended-wing-body (BWB) aircraft. This section examines the assessment and selection of aircraft design parameters, planform design, and reflex wing and conducts a complete aircraft stability analysis. A BWB aircraft conceptual design has been completed and the design. To attain static stability, it was examined and refined. The BWB aircraft's study was performed at three distinct values. The analytical findings were used to calculate the angle-of-attack (AOA) and the stall AOA. We determined the estimated initial departure angle of attack and departure region by assessing the results of the trials and a set of stability criteria.
 
Blended-Wing-Body Aircraft (BWB); Stall Departure; Static Stability; Dynamic Stability; Stability Modes; Computer-Aided-Design
 
https://wjarr.com/sites/default/files/fulltext_pdf/WJARR-2024-2961.pdf

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Lucky Bose, Isfaq Ahmed Rafsun and Junquan Fu. Research on stability for blended-wing-body aircraft. World Journal of Advanced Research and Reviews, 2024, 23(3), 2919-2932. Article DOI: https://doi.org/10.30574/wjarr.2024.23.3.2961

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