Research on stability for blended-wing-body aircraft
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Zenodo
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| Autori principali: | , , |
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| Natura: | Recurso digital |
| Lingua: | inglese |
| Pubblicazione: |
Zenodo
2024
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| _version_ | 1866901091754442752 |
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| author | Lucky Bose Isfaq Ahmed Rafsun Junquan Fu |
| author_facet | Lucky Bose Isfaq Ahmed Rafsun Junquan Fu |
| contents | <p>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.</p> |
| format | Recurso digital |
| id | zenodo_https___doi_org_10_5281_zenodo_14978810 |
| institution | Zenodo |
| language | eng |
| publishDate | 2024 |
| publisher | Zenodo |
| record_format | zenodo |
| spellingShingle | Research on stability for blended-wing-body aircraft Lucky Bose Isfaq Ahmed Rafsun Junquan Fu Blended-Wing-Body Aircraft (BWB) Stall Departure Static Stability Dynamic Stability Stability Modes Computer-Aided-Design <p>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.</p> |
| title | Research on stability for blended-wing-body aircraft |
| topic | Blended-Wing-Body Aircraft (BWB) Stall Departure Static Stability Dynamic Stability Stability Modes Computer-Aided-Design |
| url | https://doi.org/10.5281/zenodo.14978810 |