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dc.date.accessioned 2023-10-30T19:05:47Z
dc.date.available 2023-10-30T19:05:47Z
dc.date.issued 2021
dc.identifier.uri http://sedici.unlp.edu.ar/handle/10915/159599
dc.description.abstract The effects of the cyclic and collective pitch variations on a rotating blade decelerator (pararotor) wind-tunnel behavior are studied. The dynamics and aerodynamics effects of the cyclic pitch variations were studied. Starting from the Newton Euler equations, a dynamic model of the main axis dynamics is obtained. The results confirm that the cyclic pitch variations of the blades are an effective way to modify the net force and torque on the pararotor, and consequently, could be used to control pararotors with low aspect ratio blades. en
dc.language en es
dc.subject aerodinamics decelerator es
dc.subject dynamics es
dc.subject wind tunnel tests es
dc.title Effects of the cyclic and collective pitch variations on a wind-tunnel rotary-wing decelerator behavior en
dc.type Objeto de conferencia es
sedici.identifier.isbn 978-987-88-4916-4 es
sedici.creator.person Martiarena, Juan Francisco es
sedici.creator.person Nadal Mora, Vicente Javier es
sedici.creator.person Piechocki, Joaquín es
sedici.creator.person Cuerva Tejero, Álvaro es
sedici.subject.materias Ingeniería Aeronáutica es
sedici.description.fulltext true es
mods.originInfo.place Facultad de Ingeniería es
sedici.subtype Objeto de conferencia es
sedici.rights.license Creative Commons Attribution-NonCommercial-ShareAlike 4.0 International (CC BY-NC-SA 4.0)
sedici.rights.uri http://creativecommons.org/licenses/by-nc-sa/4.0/
sedici.date.exposure 2021-11
sedici.relation.event VI Congreso Argentino de Ingeniería Aeronáutica (CAIA 6) (Haedo, modalidad virtual, 17 al 19 de noviembre de 2021) es
sedici.description.peerReview peer-review es
sedici.relation.bookTitle Anales del 6° Congreso Argentino de Ingeniería Aeronáutica es


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Creative Commons Attribution-NonCommercial-ShareAlike 4.0 International (CC BY-NC-SA 4.0) Excepto donde se diga explícitamente, este item se publica bajo la siguiente licencia Creative Commons Attribution-NonCommercial-ShareAlike 4.0 International (CC BY-NC-SA 4.0)