التفاصيل البيبلوغرافية
| العنوان: |
FLOW CONTROL INVESTIGATION USING THE COANDA EFFECT ON AIRFOILS. |
| المؤلفون: |
DUMITRACHE, Alexandru, FRUNZULICA, Florin, DUMITRESCU, Horia, IONESCU, Tudor |
| المصدر: |
Scientific Research & Education in the Air Force - AFASES; 2019, Vol. 2019, p126-134, 9p |
| مصطلحات موضوعية: |
AEROFOILS, JETS (Fluid dynamics), FLOW separation |
| مستخلص: |
Numerical investigations on the flow control around airfoils, in conjunction with Coandã effect, based on RANS equations are done. The circulation control uses the tangential blowing jet on the upper surface of the airfoil near the trailing edge with the rounded or modified flatback surface. Flow field spectra around such a configurations, involving the delayed of flow separation are obtained and analyzed by CFD methods. Thus can be identified the optimum domain of the geometric and jet flow parameters in which this flow control method should be used. [ABSTRACT FROM AUTHOR] |
|
Copyright of Scientific Research & Education in the Air Force - AFASES is the property of Henri Coanda Air Force Academy and its content may not be copied or emailed to multiple sites or posted to a listserv without the copyright holder's express written permission. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract. (Copyright applies to all Abstracts.) |
| قاعدة البيانات: |
Complementary Index |
