A Linear Analysis of a Blended Wing Body (BWB) Aircraft Model
In this article a linear analysis of a Blended Wing Body (BWB) aircraft model is performed. The BWB concept is in the attention of both military and civil sectors for the fact that has reduced radar signature (in the absence of a conventional tail) and the possibility to carry more people. The trim...
| 出版年: | INCAS Bulletin |
|---|---|
| 第一著者: | |
| フォーマット: | 論文 |
| 言語: | 英語 |
| 出版事項: |
National Institute for Aerospace Research “Elie Carafoli” - INCAS
2011-09-01
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| 主題: | |
| オンライン･アクセス: | http://bulletin.incas.ro/files/state_claudia_v3_is3_full.pdf |
| _version_ | 1852815622127222784 |
|---|---|
| author | Claudia Alice STATE |
| author_facet | Claudia Alice STATE |
| author_sort | Claudia Alice STATE |
| collection | DOAJ |
| container_title | INCAS Bulletin |
| description | In this article a linear analysis of a Blended Wing Body (BWB) aircraft model is performed. The BWB concept is in the attention of both military and civil sectors for the fact that has reduced radar signature (in the absence of a conventional tail) and the possibility to carry more people. The trim values are computed, also the eigenvalues and the Jacobian matrix evaluated into the trim point are analyzed. A linear simulation in the MatLab environment is presented in order to express numerically the symbolic computations presented. The initial system is corrected in the way of increasing the consistency and coherence of the modeled type of motion and, also, suggestions are made for future work. |
| format | Article |
| id | doaj-art-57794e314af64dae94f2fea4792f672c |
| institution | Directory of Open Access Journals |
| issn | 2066-8201 2247-4528 |
| language | English |
| publishDate | 2011-09-01 |
| publisher | National Institute for Aerospace Research “Elie Carafoli” - INCAS |
| record_format | Article |
| spelling | doaj-art-57794e314af64dae94f2fea4792f672c2025-08-19T20:34:16ZengNational Institute for Aerospace Research “Elie Carafoli” - INCASINCAS Bulletin2066-82012247-45282011-09-013311512610.13111/2066-8201.2011.3.3.12A Linear Analysis of a Blended Wing Body (BWB) Aircraft ModelClaudia Alice STATEIn this article a linear analysis of a Blended Wing Body (BWB) aircraft model is performed. The BWB concept is in the attention of both military and civil sectors for the fact that has reduced radar signature (in the absence of a conventional tail) and the possibility to carry more people. The trim values are computed, also the eigenvalues and the Jacobian matrix evaluated into the trim point are analyzed. A linear simulation in the MatLab environment is presented in order to express numerically the symbolic computations presented. The initial system is corrected in the way of increasing the consistency and coherence of the modeled type of motion and, also, suggestions are made for future work.http://bulletin.incas.ro/files/state_claudia_v3_is3_full.pdfLateral-directionalBlended Wing BodyFlight Control SystemStabilitySimulation |
| spellingShingle | Claudia Alice STATE A Linear Analysis of a Blended Wing Body (BWB) Aircraft Model Lateral-directional Blended Wing Body Flight Control System Stability Simulation |
| title | A Linear Analysis of a Blended Wing Body (BWB) Aircraft Model |
| title_full | A Linear Analysis of a Blended Wing Body (BWB) Aircraft Model |
| title_fullStr | A Linear Analysis of a Blended Wing Body (BWB) Aircraft Model |
| title_full_unstemmed | A Linear Analysis of a Blended Wing Body (BWB) Aircraft Model |
| title_short | A Linear Analysis of a Blended Wing Body (BWB) Aircraft Model |
| title_sort | linear analysis of a blended wing body bwb aircraft model |
| topic | Lateral-directional Blended Wing Body Flight Control System Stability Simulation |
| url | http://bulletin.incas.ro/files/state_claudia_v3_is3_full.pdf |
| work_keys_str_mv | AT claudiaalicestate alinearanalysisofablendedwingbodybwbaircraftmodel AT claudiaalicestate linearanalysisofablendedwingbodybwbaircraftmodel |