2009
DOI: 10.1016/j.expthermflusci.2009.04.007
|View full text |Cite
|
Sign up to set email alerts
|

Experimental optimization of a free vortex propeller runner for micro hydro application

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1
1

Citation Types

2
30
0
3

Year Published

2010
2010
2024
2024

Publication Types

Select...
7
2

Relationship

1
8

Authors

Journals

citations
Cited by 70 publications
(41 citation statements)
references
References 1 publication
2
30
0
3
Order By: Relevance
“…Singh and Nestmann [2,3] investigated the influences of design parameters like the blade profile, blade height and blade number on the performance of a low head axial flow turbine for micro-hydro applications and examined the functionality of the internal performance parameters of the runner. They concluded that the blade number is a more dominating parameter than the blade height, although its variation did not result in major performance gains.…”
Section: 1mentioning
confidence: 99%
“…Singh and Nestmann [2,3] investigated the influences of design parameters like the blade profile, blade height and blade number on the performance of a low head axial flow turbine for micro-hydro applications and examined the functionality of the internal performance parameters of the runner. They concluded that the blade number is a more dominating parameter than the blade height, although its variation did not result in major performance gains.…”
Section: 1mentioning
confidence: 99%
“…However, a designer's freedom can also be exercised in choosing the values. They also concluded that having a larger hub-tip diameter ratio yielded lower runner losses [7]. From the velocity diagrams, the radial variation in the flow can be characterized at different sections along the radial coordinates of the blade equally spaced between the hub and tip locations along the length of the blade.…”
Section: (10)mentioning
confidence: 99%
“…For the given gross head of 2 m, the turbine is envisaged to work under a suction head of 1.3-1.4 m and an inlet head with 0.4-0.6 m, which eliminates the need of a closed spiral volute inlet. The volutes of other propeller researchers are closed type since their runners operate at a higher inlet head [7]. The design is based on the specifications provided by J. Susanto and S. Stamp.The open spiral volute has been adapted by [7], [3], and by Asian Phoenix Resources Ltd. in their Powerpal turbines.…”
Section: Open Spiral Volutementioning
confidence: 99%
“…Singh and Nestmann [7] carried out a series of optimization on a particular runner, that included modifications to inlet and exit tip of the blade profiles. They also developed a simple theoretical model to analyze the hydraulic phenomena due to these geometric modifications, which gave a qualitative study to the internal hydraulic phenomena.…”
Section: Introductionmentioning
confidence: 99%