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An Inverse Design Method for Cascades for Low-Reynolds Number Flow
Author
Source
Issue
Vol. 2012, Issue 2012 (31 Dec. 2012), pp.1-18, 18 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2012-06-05
Country of Publication
Egypt
No. of Pages
18
Main Subjects
Abstract EN
Inverse design of cascades for low Reynolds number can be applied for the aerodynamic development of fans and compressors.
The present contribution describes a complete design procedure by taking into account the transition from laminar to turbulent boundary layer flow.
A shape factor distribution is prescribed along the suction surface of the blades.
The inverse boundary layer calculation is performed by the application of a finite difference method.
On the pressure side the velocity distribution is prescribed in such a way that the given flow angles in front of and behind the cascade are realized.
An inverse calculation based on potential theory is applied in order to determine the geometry of the cascade.
At the end of the present contribution a cascade is designed by the described inverse design procedure and the flow is simulated by the application of CFD.
American Psychological Association (APA)
Böhle, Martin. 2012. An Inverse Design Method for Cascades for Low-Reynolds Number Flow. ISRN Applied Mathematics،Vol. 2012, no. 2012, pp.1-18.
https://search.emarefa.net/detail/BIM-449634
Modern Language Association (MLA)
Böhle, Martin. An Inverse Design Method for Cascades for Low-Reynolds Number Flow. ISRN Applied Mathematics No. 2012 (2012), pp.1-18.
https://search.emarefa.net/detail/BIM-449634
American Medical Association (AMA)
Böhle, Martin. An Inverse Design Method for Cascades for Low-Reynolds Number Flow. ISRN Applied Mathematics. 2012. Vol. 2012, no. 2012, pp.1-18.
https://search.emarefa.net/detail/BIM-449634
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-449634