Numerical optimization of helicopter rotor blade design for active twist control
The vibration of a helicopter has several different sources, such as the rotor, engine and transmission system. This creates a number of problems with performance, for example poor manoeuvrability, discomfort of the pilot, low fatigue life of the structural components, and, consequently, high operat...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
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Vilnius Gediminas Technical University
2007-09-01
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| Series: | Aviation |
| Subjects: | |
| Online Access: | https://bjrbe.vgtu.lt/index.php/Aviation/article/view/7039 |
| _version_ | 1818879024914497536 |
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| author | Andrejs Kovalovs Evgeny Barkanov Sergejs Gluhihs |
| author_facet | Andrejs Kovalovs Evgeny Barkanov Sergejs Gluhihs |
| author_sort | Andrejs Kovalovs |
| collection | DOAJ |
| description | The vibration of a helicopter has several different sources, such as the rotor, engine and transmission system. This creates a number of problems with performance, for example poor manoeuvrability, discomfort of the pilot, low fatigue life of the structural components, and, consequently, high operating costs.
First published online: 14 Oct 2010 |
| first_indexed | 2024-12-19T14:23:30Z |
| format | Article |
| id | doaj.art-92462a423e2b4dc3b7966ea40def1bec |
| institution | Directory Open Access Journal |
| issn | 1648-7788 1822-4180 |
| language | English |
| last_indexed | 2024-12-19T14:23:30Z |
| publishDate | 2007-09-01 |
| publisher | Vilnius Gediminas Technical University |
| record_format | Article |
| series | Aviation |
| spelling | doaj.art-92462a423e2b4dc3b7966ea40def1bec2022-12-21T20:17:42ZengVilnius Gediminas Technical UniversityAviation1648-77881822-41802007-09-0111310.3846/16487788.2007.9635962Numerical optimization of helicopter rotor blade design for active twist controlAndrejs Kovalovs0Evgeny Barkanov1Sergejs Gluhihs2Institute of Materials and Structures, Riga Technical University, Azenes St. 16-323, LV-1048, Riga, LatviaInstitute of Materials and Structures, Riga Technical University, Azenes St. 16-323, LV-1048, Riga, LatviaInstitute of Materials and Structures, Riga Technical University, Azenes St. 16-323, LV-1048, Riga, LatviaThe vibration of a helicopter has several different sources, such as the rotor, engine and transmission system. This creates a number of problems with performance, for example poor manoeuvrability, discomfort of the pilot, low fatigue life of the structural components, and, consequently, high operating costs. First published online: 14 Oct 2010https://bjrbe.vgtu.lt/index.php/Aviation/article/view/7039active twistmacro fibre composite (MFC)helicopter rotor bladeoptimization |
| spellingShingle | Andrejs Kovalovs Evgeny Barkanov Sergejs Gluhihs Numerical optimization of helicopter rotor blade design for active twist control Aviation active twist macro fibre composite (MFC) helicopter rotor blade optimization |
| title | Numerical optimization of helicopter rotor blade design for active twist control |
| title_full | Numerical optimization of helicopter rotor blade design for active twist control |
| title_fullStr | Numerical optimization of helicopter rotor blade design for active twist control |
| title_full_unstemmed | Numerical optimization of helicopter rotor blade design for active twist control |
| title_short | Numerical optimization of helicopter rotor blade design for active twist control |
| title_sort | numerical optimization of helicopter rotor blade design for active twist control |
| topic | active twist macro fibre composite (MFC) helicopter rotor blade optimization |
| url | https://bjrbe.vgtu.lt/index.php/Aviation/article/view/7039 |
| work_keys_str_mv | AT andrejskovalovs numericaloptimizationofhelicopterrotorbladedesignforactivetwistcontrol AT evgenybarkanov numericaloptimizationofhelicopterrotorbladedesignforactivetwistcontrol AT sergejsgluhihs numericaloptimizationofhelicopterrotorbladedesignforactivetwistcontrol |