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pro vyhledávání: '"M. Rohin Kumar"'
Autor:
Comandur Venkatesan, M. Rohin Kumar
Publikováno v:
The Aeronautical Journal. 121:637-659
For performance improvement and noise reduction, swept and anhedral tips have been incorporated in advanced-geometry rotor blades. While there are aerodynamic benefits to these advanced tip geometries, they come at the cost of complicated structural
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a82759bf7eadcb77bda1dcdc681b55eb
https://doi.org/10.1017/aer.2017.15
https://doi.org/10.1017/aer.2017.15
Autor:
M. Rohin Kumar, Comandur Venkatesan
Publikováno v:
The Aeronautical Journal. 120:271-290
The influence of the blade geometric parameters on the structural dynamic characteristics, response and loads of a helicopter rotor under hover condition in a whirl tower was investigated. A general geometry was considered for the rotor blade which i
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::511fcc38f6c318774e7711298fcd63e8
https://doi.org/10.1017/aer.2015.11
https://doi.org/10.1017/aer.2015.11
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