Aerodynamic Design of a Transonic Axial Fan with Low Aspect Ratio and Validating

Q: How can I download an article?

To download an article from SID, first log in to the site, search for the article title, and click on the 'Download Article' option.

Q: How can I download an ISI article?

To download an ISI article on SID, enter the keyword or article title in the search bar, view the relevant results, click on the desired article, and select the 'Download Article' option.

Q: How can I access the SID database?

To access the SID database, visit SID.ir, create an account, and log in to access scientific resources.

Q: Is downloading articles from SID free?

Some articles on SID are available for free, while others require payment. Details are specified on the article's page.

ABBASI S.

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Journal Paper

Paper Information

Journal: JOURNAL OF SOLID AND FLUID MECHANICS Year:2019 | Volume:9 | Issue:1 Page(s): 251-264

Download Full-Text

Persian Verion

View:

244

Download:

Cites:

Information Journal Paper

Title

Aerodynamic Design of a Transonic Axial Fan with Low Aspect Ratio and Validating

Author(s)

ABBASI S. | Issue Writer Certificate

Keywords

Aerodynamic DesignQ2

Axial FanQ1

Low Aspect RatioQ1

Transonic RegimeQ1

Abstract

In recent years trends towards designing Axial Fan with Low Aspect Ratio have been increased. Application of this kind of blades leads to higher rotor efficiency relative to blade with high aspect ratios. In contrast, applying this kind of blade causes to intensify 3D flows, increasing secondary losses and creating losses due to shock occurrence. In the current study, designing of a two stage Axial Fan with Low Aspect Ratio is carried out. To obtain losses in the Axial Fan, appropriate models have been employed for profile loss, secondary loss shock loss and tip clearance loss. For extracting blade’ s profile, polynomial camber and naca 65 thickness distribution have been used. Comparing the obtained results including loss estimation, meridional velocity, pressure and diffusion factor distribution and blade geometrical parameters such as stagger angle, chord length, solidity and camber angle show good agreement. The 3D shape of the blade have been extracted by calculating the stagger angle and thickness distribution in each section.

Cites

No record.

References

No record.

Cite

APA: Copy

ABBASI, S.. (2019). Aerodynamic Design of a Transonic Axial Fan with Low Aspect Ratio and Validating. JOURNAL OF SOLID AND FLUID MECHANICS, 9(1 ), 251-264. SID. https://sid.ir/paper/368893/en

Vancouver: Copy

ABBASI S.. Aerodynamic Design of a Transonic Axial Fan with Low Aspect Ratio and Validating. JOURNAL OF SOLID AND FLUID MECHANICS[Internet]. 2019;9(1 ):251-264. Available from: https://sid.ir/paper/368893/en

IEEE: Copy

S. ABBASI, “Aerodynamic Design of a Transonic Axial Fan with Low Aspect Ratio and Validating,” JOURNAL OF SOLID AND FLUID MECHANICS, vol. 9, no. 1 , pp. 251–264, 2019, [Online]. Available: https://sid.ir/paper/368893/en

Related Journal Papers