Academic Journal
Experimental Investigation of the Flow Field around NACA0012 Airfoil
| العنوان: | Experimental Investigation of the Flow Field around NACA0012 Airfoil |
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| المؤلفون: | Yemenici, Onur |
| المصدر: | International Journal of Sciences, Volume 2(2013-08), 98-101, (2013-08-26) |
| بيانات النشر: | Zenodo |
| سنة النشر: | 2013 |
| المجموعة: | Zenodo |
| الوصف: | In this study, an experimental investigation of the flow field around NACA0012 airfoil was carried out in a wind tunnel under the effects of the Reynolds number and angle of attack. The Reynolds number based on the chord length of airfoil and the attack angle was varied from 9.7x104 to 1.9x105 and 0 to 140 respectively. Mean velocities were measured by a constant temperature anemometer and static pressures by a micro-manometer. The results showed that the pressure and lift coefficients displayed a strong dependence on Reynolds number and attack angle. Read Complete Article at ijSciences: V2201307242 |
| نوع الوثيقة: | article in journal/newspaper |
| اللغة: | English |
| Relation: | https://doi.org/10.5281/zenodo.3348421; https://doi.org/10.5281/zenodo.3348422; oai:zenodo.org:3348422; https://www.ijsciences.com/pub/article/242 |
| DOI: | 10.5281/zenodo.3348422 |
| الاتاحة: | https://doi.org/10.5281/zenodo.3348422 https://www.ijsciences.com/pub/article/242 https://www.ijsciences.com/pub/pdf/V2-201308-21.pdf |
| Rights: | info:eu-repo/semantics/openAccess ; Creative Commons Attribution 4.0 International ; https://creativecommons.org/licenses/by/4.0/legalcode |
| رقم الانضمام: | edsbas.2CCD4D7B |
| قاعدة البيانات: | BASE |
| DOI: | 10.5281/zenodo.3348422 |
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