Mehmet Metin Yavuz

E-mail

ymetin@metu.edu.tr

Department

Department of Mechanical Engineering

ORCID

0000-0002-9491-4115

Scopus Author ID

35110257400

Web of Science Researcher ID

AAQ-5164-2020

Material modeling and recent findings in transcatheter aortic valve implantation simulations Mutlu, Onur; Saribay, Murat; Yavuz, Mehmet Metin; Salman, Huseyin Enes; Al-Nabti, A.Rahman D.M.H.; Yalcin, Huseyin Cagatay (2024-10-01) Background and objective: Transcatheter aortic valve implantation (TAVI) has significantly transformed the management of aortic valve (AV) diseases, presenting a minimally invasive option compared to traditional surgical v...
Method development for estimation of bleed momentum coefficient using surface pressure measurements and in situ hot wire calibration Çetin, Cenk; Yavuz, Mehmet Metin (2024-07-01) Recently, as a passive flow control method, bleeding technique allowing flow of upstream towards suction side by interior passages, has been utilized on non-slender delta wing planforms, where effective geometries can enha...
Experimental investigation of dynamic ground boundary condition for a non-slender delta wing Koçak, Göktuğ; Yavuz, Mehmet Metin (2024-01-01) In this paper, the ground boundary condition was studied for static ground effect (SGE) of a non-slender delta wing with sweep angle of 45 degree in a low-speed wind tunnel at Reynolds number of 9x104 considering static gr...
Effect Of Inlet Velocity Profıle And Entrance Length On Abdominal Aortic Aneurysm Hemodynamics Simulations Ramazanlı, Burcu; Sert, Cüneyt; Yavuz, Mehmet Metin (2023-01-01) In computational Abdominal Aortic Aneurysm (AAA) hemodynamics studies, along with adjusting the problem geometry, mesh, transport, turbulence and rheology models; setting up boundary conditions (BC) is also a very importan...
Effect of ground on aerodynamics and longitudinal static stability of a non-slender delta wing Koçak, Göktuğ; Yavuz, Mehmet Metin (2022-11-01) © 2022 Elsevier Masson SASIn this paper, the effect of ground on aerodynamics and longitudinal static stability of a non-slender delta wing with sweep angle of 45 degree and thickness-to-chord ratio (t/c) of 5.9% was chara...
PASİF AKITMA TEKNİĞİNİN İNCE OLMAYAN BİR DELTA KANADIN AERODİNAMİK PERFORMANSINA ETKİSİNİN YER ETKİSİ DURUMUNDA İNCELENMESİ Yılmaz, Oğuzhan; Aktaş, Murat Kadri; Yavuz, Mehmet Metin (2022-09-14)
Yeni bir pasif akıtma tasarımı ile düşük ok açılı delta kanat akışının kontrolü Çetin, Cenk; Koçak, Göktuğ; Yavuz, Mehmet Metin (2022-09-14) Düşük hızlı rüzgâr tünelinde sürdürülen bu deneysel çalışmada, 45 derece ok açısına sahip bir delta kanat üzerinde oluşan akış yapılarının yeni bir pasif akıtma deliği tasarımı ile kontrolü gerçekleştirilmiştir. Kanat yüze...
Düşük ok açılı delta ve ters delta kanatların aerodinamiği: kanat kalınlığı etkisi Koçak, Göktuğ; Yavuz, Mehmet Metin (2022-09-14) Bu çalışmada düşük ok açılı delta ve ters delta kanatların aerodinamik özellikleri farklı kanat kalınlığı oranında (𝑡/𝑐) kuvvet ölçümleri ile incelenmiştir. Deneyler 45 derece ok açısına sahip 4 farklı kanat kullanılarak...
Aerodynamics of non-slender delta and reverse delta wings: Wing thickness, anhedral angle and cropping ratio KOÇAK, Göktuğ; Yavuz, Mehmet Metin (2022-01-01) © 2022 Chinese Society of Aeronautics and AstronauticsThe effects of thickness-to-chord (t/c) ratio, anhedral angle (δ), and cropping ratio from trailing-edge (Cr%) on the aerodynamics of non-slender reverse delta wings in...
Analysis of flow structure in a helicopter cabin to improve the thermal comfort using cfd modeling Şahin, Doruk; Yavuz, Mehmet Metin (null; 2019-09-20) Proper distribution of conditioned air inside the cabins of passenger transportation type aircrafts is crucial in terms of passengers? comfort. In the present study, computational fluid dynamics (CFD) models are developed ...

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