A correction factor for pressure distribution analysis of an aerofoil in a subsonic flow
Joint Authors
Abu Darraj, Sakhr B.
Sail, Khalid H.
Source
Journal of Science and Technology
Issue
Vol. 9, Issue 1 (31 Dec. 2008), pp.1-16, 16 p.
Publisher
Sudan University of Science and Technology Deanship of Scientific Research
Publication Date
2008-12-31
Country of Publication
Sudan
No. of Pages
16
Main Subjects
Topics
Abstract EN
This study investigates the gِِeometrical solution for a given pressure (i.e.
velocity) distribution of subsonic flow around an aerofoil section using an analytical method.
The results show that the analytical method is not precise on the leading edge, when it is used to solve the mean camber line of updated profile RAE (Royal Aircraft Establishment).
Therefore, a correction parameter with changeable values ranging between 0.32 and 0.42 was created, and it gives appropriate results.
American Psychological Association (APA)
Sail, Khalid H.& Abu Darraj, Sakhr B.. 2008. A correction factor for pressure distribution analysis of an aerofoil in a subsonic flow. Journal of Science and Technology،Vol. 9, no. 1, pp.1-16.
https://search.emarefa.net/detail/BIM-299578
Modern Language Association (MLA)
Sail, Khalid H.& Abu Darraj, Sakhr B.. A correction factor for pressure distribution analysis of an aerofoil in a subsonic flow. Journal of Science and Technology Vol. 9, no. 1 (2008), pp.1-16.
https://search.emarefa.net/detail/BIM-299578
American Medical Association (AMA)
Sail, Khalid H.& Abu Darraj, Sakhr B.. A correction factor for pressure distribution analysis of an aerofoil in a subsonic flow. Journal of Science and Technology. 2008. Vol. 9, no. 1, pp.1-16.
https://search.emarefa.net/detail/BIM-299578
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references : p. 16
Record ID
BIM-299578
