Numerical analysis of the influence of particular autogyro parts on the aerodynamic forces
This paper describes the research gyrocopter and presents the methodology of numerical calculations for this type of research objects. There are also the results of an ANSYS Fluent three-dimensional simulation of an airflow around a gyrocopter, excluding an airflow around its main rotor and propelle...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
EDP Sciences
2017-01-01
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| Series: | ITM Web of Conferences |
| Online Access: | https://doi.org/10.1051/itmconf/20171507008 |
| _version_ | 1818572869338136576 |
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| author | Czyż Zbigniew Karpiński Paweł Łusiak Tomasz Szczepanik Tomasz |
| author_facet | Czyż Zbigniew Karpiński Paweł Łusiak Tomasz Szczepanik Tomasz |
| author_sort | Czyż Zbigniew |
| collection | DOAJ |
| description | This paper describes the research gyrocopter and presents the methodology of numerical calculations for this type of research objects. There are also the results of an ANSYS Fluent three-dimensional simulation of an airflow around a gyrocopter, excluding an airflow around its main rotor and propeller blades. The calculations enabled basic aerodynamic characteristics. The analysis of the numerical calculations focuses on the impact of gyrocopter individual sections like a fuselage, tail, tail boom, etc., on aerodynamic forces and moments, as well as coefficients of aerodynamic forces and moments. The research scope covers an angle of attack α ranging between -20° and 25° at a sideslip angle equal to 0. |
| first_indexed | 2024-12-15T00:03:24Z |
| format | Article |
| id | doaj.art-60d43cdf266745e093b0a338d1567dd2 |
| institution | Directory Open Access Journal |
| issn | 2271-2097 |
| language | English |
| last_indexed | 2024-12-15T00:03:24Z |
| publishDate | 2017-01-01 |
| publisher | EDP Sciences |
| record_format | Article |
| series | ITM Web of Conferences |
| spelling | doaj.art-60d43cdf266745e093b0a338d1567dd22022-12-21T22:42:50ZengEDP SciencesITM Web of Conferences2271-20972017-01-01150700810.1051/itmconf/20171507008itmconf_cmes-17_07008Numerical analysis of the influence of particular autogyro parts on the aerodynamic forcesCzyż ZbigniewKarpiński PawełŁusiak TomaszSzczepanik TomaszThis paper describes the research gyrocopter and presents the methodology of numerical calculations for this type of research objects. There are also the results of an ANSYS Fluent three-dimensional simulation of an airflow around a gyrocopter, excluding an airflow around its main rotor and propeller blades. The calculations enabled basic aerodynamic characteristics. The analysis of the numerical calculations focuses on the impact of gyrocopter individual sections like a fuselage, tail, tail boom, etc., on aerodynamic forces and moments, as well as coefficients of aerodynamic forces and moments. The research scope covers an angle of attack α ranging between -20° and 25° at a sideslip angle equal to 0.https://doi.org/10.1051/itmconf/20171507008 |
| spellingShingle | Czyż Zbigniew Karpiński Paweł Łusiak Tomasz Szczepanik Tomasz Numerical analysis of the influence of particular autogyro parts on the aerodynamic forces ITM Web of Conferences |
| title | Numerical analysis of the influence of particular autogyro parts on the aerodynamic forces |
| title_full | Numerical analysis of the influence of particular autogyro parts on the aerodynamic forces |
| title_fullStr | Numerical analysis of the influence of particular autogyro parts on the aerodynamic forces |
| title_full_unstemmed | Numerical analysis of the influence of particular autogyro parts on the aerodynamic forces |
| title_short | Numerical analysis of the influence of particular autogyro parts on the aerodynamic forces |
| title_sort | numerical analysis of the influence of particular autogyro parts on the aerodynamic forces |
| url | https://doi.org/10.1051/itmconf/20171507008 |
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