PRELIMINARY RESULTS FROM THE SHROUDED WIND-TURBINE PILOT PLANT.

Ozer Igra

doi:10.2514/3.48024

PRELIMINARY RESULTS FROM THE SHROUDED WIND-TURBINE PILOT PLANT.

Ozer Igra

Department of Mechanical Engineering

Research output: Contribution to journal › Article › peer-review

2 Scopus citations

Abstract

A shrouded wind turbine was built, to be tested in the 3. 6 multiplied by 2. 6 test sections of the subsonic wind tunnel of the Israel Aircraft Industry. The shroud housed a 40 cm turbine composed of a seven-blade stator preceded by a two-, three-, four-, six-, or eight-blade rotor. Without using a ring-shaped flap, an augmentation factor of about two was obtained. The turbine was designed for 5 m/s wind. With such a wind, its expected output was about 1 hp. The results obtained during the first three months of operation are given in the following section.

Original language	English
Pages (from-to)	190-192
Number of pages	3
Journal	Journal of energy
Volume	4
Issue number	4
DOIs	https://doi.org/10.2514/3.48024
State	Published - 1 Jan 1980

UN SDGs

This output contributes to the following UN Sustainable Development Goals (SDGs)

SDG 7 Affordable and Clean Energy

ASJC Scopus subject areas

General Engineering

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Cite this

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title = "PRELIMINARY RESULTS FROM THE SHROUDED WIND-TURBINE PILOT PLANT.",

abstract = "A shrouded wind turbine was built, to be tested in the 3. 6 multiplied by 2. 6 test sections of the subsonic wind tunnel of the Israel Aircraft Industry. The shroud housed a 40 cm turbine composed of a seven-blade stator preceded by a two-, three-, four-, six-, or eight-blade rotor. Without using a ring-shaped flap, an augmentation factor of about two was obtained. The turbine was designed for 5 m/s wind. With such a wind, its expected output was about 1 hp. The results obtained during the first three months of operation are given in the following section.",

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N2 - A shrouded wind turbine was built, to be tested in the 3. 6 multiplied by 2. 6 test sections of the subsonic wind tunnel of the Israel Aircraft Industry. The shroud housed a 40 cm turbine composed of a seven-blade stator preceded by a two-, three-, four-, six-, or eight-blade rotor. Without using a ring-shaped flap, an augmentation factor of about two was obtained. The turbine was designed for 5 m/s wind. With such a wind, its expected output was about 1 hp. The results obtained during the first three months of operation are given in the following section.

AB - A shrouded wind turbine was built, to be tested in the 3. 6 multiplied by 2. 6 test sections of the subsonic wind tunnel of the Israel Aircraft Industry. The shroud housed a 40 cm turbine composed of a seven-blade stator preceded by a two-, three-, four-, six-, or eight-blade rotor. Without using a ring-shaped flap, an augmentation factor of about two was obtained. The turbine was designed for 5 m/s wind. With such a wind, its expected output was about 1 hp. The results obtained during the first three months of operation are given in the following section.

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PRELIMINARY RESULTS FROM THE SHROUDED WIND-TURBINE PILOT PLANT.

Abstract

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