SİLİNDİRİK ENJEKSİYON DELİKLERİNDE FİLM SOĞUTMA İNCELEMESİ

This paper deals with experimental and numerical investigation of the film cooling effectiveness on a flat plate. Eleven injection holes on the model are in a single row. The holes have cylindrical cross section and they are 8.5 mm diameters. The injection angle is 30o. The blowing ratios vary fro...

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Bibliographic Details
Main Author: İbrahim Koç
Format: Article
Language:English
Published: Turkish Air Force Academy 2006-07-01
Series:Havacılık ve Uzay Teknolojileri Dergisi
Subjects:
Online Access:http://www.jast.hho.edu.tr/JAST/index.php/JAST/article/view/141/129
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author İbrahim Koç
author_facet İbrahim Koç
author_sort İbrahim Koç
collection DOAJ
description This paper deals with experimental and numerical investigation of the film cooling effectiveness on a flat plate. Eleven injection holes on the model are in a single row. The holes have cylindrical cross section and they are 8.5 mm diameters. The injection angle is 30o. The blowing ratios vary from 0.5 to 2.0. The experiments and their computational models have been established to investigate their effects at 57 oC injection temperature and different blowing ratios. . The experimental and computational solutions show the blowing ratio affect on film cooling effectiveness and a suitable blowing ratio should be selected for good film cooling performance in both mainstream and lateral direction. In the current study, the best blowing ratio is 0.5. In additon, when the blowing ratio is increased the film cooling effectiveness deacreases.
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spelling doaj.art-bdd7c0b1e10548e182df057295da24352023-02-15T16:14:19ZengTurkish Air Force AcademyHavacılık ve Uzay Teknolojileri Dergisi1304-04481304-04482006-07-012416SİLİNDİRİK ENJEKSİYON DELİKLERİNDE FİLM SOĞUTMA İNCELEMESİİbrahim Koç0Turkish Air Force AcademyThis paper deals with experimental and numerical investigation of the film cooling effectiveness on a flat plate. Eleven injection holes on the model are in a single row. The holes have cylindrical cross section and they are 8.5 mm diameters. The injection angle is 30o. The blowing ratios vary from 0.5 to 2.0. The experiments and their computational models have been established to investigate their effects at 57 oC injection temperature and different blowing ratios. . The experimental and computational solutions show the blowing ratio affect on film cooling effectiveness and a suitable blowing ratio should be selected for good film cooling performance in both mainstream and lateral direction. In the current study, the best blowing ratio is 0.5. In additon, when the blowing ratio is increased the film cooling effectiveness deacreases.http://www.jast.hho.edu.tr/JAST/index.php/JAST/article/view/141/129Film CoolingFilm Cooling EffectivenessNumerical InvestigationExperimental InvestigationBlowing ratio
spellingShingle İbrahim Koç
SİLİNDİRİK ENJEKSİYON DELİKLERİNDE FİLM SOĞUTMA İNCELEMESİ
Havacılık ve Uzay Teknolojileri Dergisi
Film Cooling
Film Cooling Effectiveness
Numerical Investigation
Experimental Investigation
Blowing ratio
title SİLİNDİRİK ENJEKSİYON DELİKLERİNDE FİLM SOĞUTMA İNCELEMESİ
title_full SİLİNDİRİK ENJEKSİYON DELİKLERİNDE FİLM SOĞUTMA İNCELEMESİ
title_fullStr SİLİNDİRİK ENJEKSİYON DELİKLERİNDE FİLM SOĞUTMA İNCELEMESİ
title_full_unstemmed SİLİNDİRİK ENJEKSİYON DELİKLERİNDE FİLM SOĞUTMA İNCELEMESİ
title_short SİLİNDİRİK ENJEKSİYON DELİKLERİNDE FİLM SOĞUTMA İNCELEMESİ
title_sort silindirik enjeksiyon deliklerinde film sogutma incelemesi
topic Film Cooling
Film Cooling Effectiveness
Numerical Investigation
Experimental Investigation
Blowing ratio
url http://www.jast.hho.edu.tr/JAST/index.php/JAST/article/view/141/129
work_keys_str_mv AT ibrahimkoc silindirikenjeksiyondeliklerindefilmsogutmaincelemesi