Duyurular & Dokümanlar

Tez Dosyaları 11

Characterization of flow structure and wall shear stress in patient-specific healthy and aneurysmal abdominal aorta phantoms using particle image velocimetry

830538.pdf Creative Commons License

Control of leading edge vortex and three-dimensional surface separation on a non-slender delta wing using passive and active techniques

911191.pdf Creative Commons License

Thermal comfort analysis of military aircraft cabin using computational fluid dynamics

763694.pdf Creative Commons License

Simulation of aneurysm hemodynamics to predict intraluminal thrombus formation region

772000.pdf Creative Commons License

Control of flow structure on non-slender delta wing using bio inspired edge modifications

974940.pdf Creative Commons License

Effect of thickness-to-chord ratio on flow structure of a low swept delta wing

489535.pdf Creative Commons License

Control of flow structure on low swept delta wing with steady leading edge blowing

378002.pdf Creative Commons License

Characterization of wall shear stress in abdominal aortic aneurysm phantom using particle image velocimetry

693806.pdf Creative Commons License

Effect of ground on flow structure of non-slender delta and reverse delta wings

782011.pdf Creative Commons License

BİR HELİKOPTER KABİNİNDE TERMAL KONFORU İYİLEŞTİRME AMACIYLA AKIŞ YAPISININ HESAPLAMALI AKIŞKANLAR DİNAMİĞİ MODELLEME İLE İNCELENMESİ

504539.pdf Creative Commons License

Characterization of vortex ring in abdominal aortic aneurysm phantom using particle image velocimetry

693805.pdf Creative Commons License