Zobrazeno 1 - 10
of 10
pro vyhledávání: '"Şumnu, Ahmet"'
Autor:
ŞUMNU, Ahmet1 ahmet.sumnu@iste.edu.tr, GÜZELBEY, İbrahim Halil2
Publikováno v:
Journal of Thermal Engineering. Sep2023, Vol. 9 Issue 5, p1260-1271. 12p.
Autor:
Şumnu, Ahmet
Publikováno v:
International Journal of Automotive and Mechanical Engineering. 19:10063-10072
In the current study, numerical analysis of passive control flow with a control rod for Ahmed body is performed at different slant angles and velocities and placed rod locations on the slant surface. The aim of the study is to improve aerodynamic per
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::59fec54c90bf7dd04f2f6a715351963f
https://doi.org/10.15282/ijame.19.4.2022.03.0777
https://doi.org/10.15282/ijame.19.4.2022.03.0777
Autor:
Şumnu, Ahmet1 ahmet.sumnu@iste.edu.tr
Publikováno v:
Nigde Omer Halisdemir University Journal of Engineering Sciences / Niğde Ömer Halisdemir Üniversitesi Mühendislik Bilimleri Dergisi. 2021, Vol. 10 Issue 2, p824-832. 9p.
Publikováno v:
International Journal of Aerospace Engineering. 6/8/2020, p1-17. 17p.
Autor:
ŞUMNU, Ahmet
Publikováno v:
Volume: 37, Issue: 3 813-826
Cukurova University Journal of the Faculty of Engineering
Çukurova Üniversitesi Mühendislik Fakültesi Dergisi
Cukurova University Journal of the Faculty of Engineering
Çukurova Üniversitesi Mühendislik Fakültesi Dergisi
In the present study, effect of side devices and crosswind flow are investigated to observe aerodynamic drag coefficient for a simplified ground vehicle (Ahmed body) since it directly effects fuel consumption. When the literature was examined, the st
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=tubitakulakb::f0adda3631592348ce3f578756e59b2f
https://dergipark.org.tr/tr/pub/cukurovaumfd/issue/73044/1190585
https://dergipark.org.tr/tr/pub/cukurovaumfd/issue/73044/1190585
Autor:
Şumnu, Ahmet, Güzelbey, İbrahim Halil
The wing of missile can be considered as an effective factor for determination of lift to drag ratio. However, there are few studies that investigate wing effect on missile aerodynamics. Therefore, the purpose of this study is to indicate wing effect
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______4723::3735e4581032c7331c6cbe4c3560fe1e
https://hdl.handle.net/20.500.12508/1925
https://hdl.handle.net/20.500.12508/1925
Autor:
Şumnu, Ahmet
Bu çalışmada, füze dış geometrisini değiştirerek aerodinamik performansı iyileştirmek ve süpersonik hızlarda şekil optimizasyonunun füze performansı üzerindeki etkilerini araştırmak için aerodinamik şekil optimizasyonu yapılmakta
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od_____10208::ca56d1920d34f1c2f01e8110602d0a5d
https://acikbilim.yok.gov.tr/handle/20.500.12812/423703
https://acikbilim.yok.gov.tr/handle/20.500.12812/423703
Autor:
Şumnu, Ahmet
Bu çalışmada, doğrusal motor kullanılan bir Stewart platformun kinematik ve dinamik analizi ve kontrolü gerçekleştirilmektedir. Bu çalışmanın amacı doğrusal motor kullanarak yüksek ivme, hız elde etmek ve verimliliği arttırmaktır.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od_____10208::8283544186fe23123238a0555a2ef06d
https://acikbilim.yok.gov.tr/handle/20.500.12812/427042
https://acikbilim.yok.gov.tr/handle/20.500.12812/427042
Akademický článek
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Publikováno v:
Journal of Aeronautics & Space Technologies / Havacilik ve Uzay Teknolojileri Dergisi. 2018, Vol. 11 Issue 2, p9-16. 8p.