CFD Case Study on a Nozzle Flow: Literature Review, Theoretical Framework, Tools and Educational Aspects
Yazarlar (3)
Ali Huseyin Abdulkareem
Dr. Öğr. Üyesi Eyüb Canlı Selçuk Üniversitesi, Türkiye
Prof. Dr. Ali ATEŞ Selçuk Üniversitesi, Türkiye
| Bildiri Türü |
Tebliğ/Bildiri
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Bildiri Dili | İngilizce |
| Bildiri Alt Türü | Tam Metin Olarak Yayınlanan Tebliğ (Uluslararası Kongre/Sempozyum) | ||
| Bildiri Niteliği | Alanında Hakemli Uluslararası Kongre/Sempozyum | ||
| Kongre Adı | International Conference on Engineering Technologies (ICENTE’18) | ||
| Kongre Tarihi | 26-10-2018 / 28-10-2018 | ||
| Basıldığı Ülke | Türkiye | Basıldığı Şehir | Konya |
| Bildiri Linki | http://icente.selcuk.edu.tr/uploads/files2/ICENTE18_proceedingsbookv3.pdf | ||
| UAK Araştırma Alanları |
Isı Transferi
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| Özet |
| State of art engineering involves lots of software types and numbers. The theoretical framework on a vocation is not sufficient for today’s undergraduates to integrate into the industry. Therefore, engineering programs are implementing courses on related software types. This work focuses on particular and widespread Computational Fluid Dynamics software in respect of mechanical engineering education. A case was determined which involved a nozzle flow analysis. Particular attention was paid on recent works for the case and for the related education studies. After a theoretical framework section containing governing equations of the physical phenomena, a section is dedicated on the used software tool. Subsequently, a results section is provided on case results and this section also includes evaluation of the results in terms of undergraduate education of mechanical engineering. Finally some concluding remarks are listed. As a major conclusion, skills on using software and skills on understanding and evaluating results in respect of engineering should be separated from each other and should be subject of different courses. The two dimensional CFD analysis results show that the analysis is in agreement with real world physics. The static pressure values ranged between-88120 Pa gauge pressure and 286200 Pa gauge pressure while Mach Number ranged between 0.15 to 2.85. |
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