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International Journal of Engineering، جلد ۲۹، شماره ۴، صفحات ۵۵۴-۵۶۲
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| عنوان فارسی |
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| چکیده فارسی مقاله |
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| کلیدواژه‌های فارسی مقاله |
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| عنوان انگلیسی |
Towards an Analytical Model for Film Cooling Prediction using Integral Turbulent Boundary layer |
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| چکیده انگلیسی مقاله |
The objective of this work is to develop deep theoretical methods that are based on the solution of the integral boundary layer equations for investigating film cooling in liquid rocket engine. The integral model assumes that heat is transferred from hot free stream gas to the liquid film both by convection and radiation. The mass is transferred to the free srteam gas by the well-known blowing process. Downstream of the liquid film, the gas effectiveness is obtained by solving boundary layer integral equations. It incorporates a differential model for calorimeter mixing between liquid vapors in the boundary layer with the free stream gas entrained in the boundary layer. Comparisons with existing theoretical and experimental results indicate the film coating trends were well predicted by the present integral model proposed by us. |
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| کلیدواژه‌های انگلیسی مقاله |
Film, cooling, Analytical, heat transfer, Rocket, model |
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| نویسندگان مقاله |
Yash Agrawal |
Mechanical Engineering, Amity University Uttar Pradesh Noida
Abhimanyu Bhadauria |
Mechanical Engineering , Amity University Uttar Pradesh Noida
basant Sikarwar |
Mechanical Engineering, Amity University Uttar Pradesh Noida India
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| نشانی اینترنتی |
http://www.ije.ir/article_72708_cdce1e210af489ab6e90b4cf1f307fff.pdf |
| فایل مقاله |
اشکال در دسترسی به فایل - ./files/site1/rds_journals/409/article-409-2062337.pdf |
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| زبان مقاله منتشر شده |
en |
| موضوعات مقاله منتشر شده |
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