Estudo experimental de uma família de rotores tipo hélice

The Power Coefficient, Torque Coefficient and Thrust Coefficient was derived from the data collected using 20 models of 3 blades propeller wind rotors tested in a wind tunnel. The rotor analysed had untwisted blades of constant chord and the sarne profile – Go 624. The models used had a 0,45m diameter and the square test section of the wind tunnel an area of l m2 • The maximum wind speed was around 9,0 m/s.

Grantor dc:publisher

Universidade Federal do Rio de Janeiro

Year dc:date.issued

1985

Author dc:creator

• Rischbieter, Ivo

Advisor dc:contributor.advisor

• Hirata, Miguel Hiroo

• Rotores
• Fluidodinâmica
• Termodinâmica

Statement dc:rights

• Acesso Aberto

Language dc:language

por

Handle dc:identifier.uri

http://hdl.handle.net/11422/4268

OAI identifier oai:identifier

oai:pantheon.ufrj.br:11422/4268