Katı yakıtlı roket motorlarında kullanılan atılabilir lüle sistemlerinin kavramsal fazda deneysel ve sayısal olarak incelenmesi

Date

2022-09-15

Author

Aysan, Mehmet Safa
Başkan Perçin, Özge

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This work is licensed under a Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.

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URI

https://hdl.handle.net/11511/99861

Conference Name

9. Ulusal Havacılık ve Uzay Konferansı

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Department of Aerospace Engineering, Conference / Seminar

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Katı yakıtlı roket motorlarında üç boyutlu yakıt gerilemesi ile akışın modellenmesi Aksel, Haluk M.; Coşkun, Korhan; Toker, Atılgan; Tınaztepe, Tuğrul(2008) Katı yakıtlı roket motorlarının performansını motor içinde yapılan aerodinamik hesaplamalarla elde etmek mümkündür. Bu amaçla motor içerisindeki katı yakıtın geriye doğru yanması ve motor ile lüle içerisindeki iç akışın modellenmesi gerekmektedir. Akış hesaplarının yapılacağı kontrol hacminin oluşturulabilmesi için geriye yanma hesaplarının yapılması gerekmektedir. Katı yakıtın yanması esnasında katı ve gaz fazları arasında kalan ara yüzey, yakıta doğru yüzeye normal yönde hareket ederken...
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Citation Formats

M. S. Aysan and Ö. Başkan Perçin, “Katı yakıtlı roket motorlarında kullanılan atılabilir lüle sistemlerinin kavramsal fazda deneysel ve sayısal olarak incelenmesi,” presented at the 9. Ulusal Havacılık ve Uzay Konferansı, İzmir, Türkiye, 2022, Accessed: 00, 2022. [Online]. Available: https://hdl.handle.net/11511/99861.