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Improving the Load Carrying Capacity of Highly Tapered Laminates
Ergin, Fırat; Kayran, Altan (2024-02-08)
Kat düşme bölgelerindeki artan gerilimler, katman ayrılmasına neden olur ve çok sayıda katın kısa mesafede sonlandırıldığı kompozit parçaların mukavemetini azaltır. Bu çalışmada, yüksek oranda konikleştirilmiş lamine kompo...
Design and Analysis of a Small-Scale Solar Powered UAV
ANILIR, BERKAN; Afzal, Aftab; Said Al Abri, Omar Khalifa; Khamis Al Dhafari, Luqman Sulaiman; Khan, Abid Ali; Kurtuluş, Dilek Funda (2023-12-16)
Observation of heterogeneous deformation microstructure in ECAP processing of high-purity niobium
Ikeda, Satoshi; Miyamoto, Hiroyuki; Yuasa, Motohito; Yalçınkaya, Tuncay; Bulut, Orhun; Günay, Enes (2023-11-28)
The Three-dimensional Flows around Tip-vortex Cavities in the Wake of a Ship Propeller
Başkan Perçin, Özge; FISCALETTI, DANIELE; ELSINGA, GERRIT; VAN TERWISGA, TOM (2023-10-26)
Katman Azaltma Bölgelerinde katman Ayrılması Başlangıcının Geciktirilmesinde Kalınlık Boyunca Basınç Gerilmesinin Uygulanması
Ergin, Fırat; Kayran, Altan (2023-10-06)
Kat sonlandırma bölgeleri, havacılık ve uzay endüstrisinde kullanılan lamine kompozit yapıların kaçınılmaz parçalarıdır ve yapıdaki malzeme süreksizliklerinden dolayı hasarın erken başlamasından sorumludurlar. Bu nedenle k...
Future of Unmanned Power Aerial Vehicles
Kurtuluş, Dilek Funda (2023-10-03)
A Bio-Inspired Control Approach for 3D Flapping-Flight
Çalış, Özgün; ARIKAN, KUTLUK BİLGE; Kurtuluş, Dilek Funda (2023-10-03)
Estimating Sweet Spot for UAV Formation Flight Using Vortex Lattice Method and Machine Learning
Tatar, Umutcan; Kahveci, Harika Senem (2023-09-15)
Experimental Analysis of a Boundary Layer Ingestion Propulsion System with a Counter-Rotating Propulsor
BİLYAZ, İBRAHİM SONER; Başkan Perçin, Özge (2023-09-15)
Numerical Investigation of the Effect of Winglets on the Flying Qualities of an Aircraft
ALA, ASLINUR; Başkan Perçin, Özge (2023-09-15)
Topaklanabilir nano-katkı içeren nanokompozitlerin gömülü eleman yöntemiyle homojenleştirilmesi
Demirtaş, Alperen; Gürses, Ercan (2023-09-14)
Nanocomposites are materials that consist of matrix and nano inclusions as reinforcement. Aside aforementioned two phases, nanoparticles can agglomerate and construct a new phase with different mechanical and geometrical ...
Yüksek Konik Laminatlarda Katman Ayrılmasının İncelenmesi
Ergin, Fırat; Kayran, Altan (2023-09-14)
Lamine bir kompozit parçadaki çok sayıda ardışık kat sonlandırması, oldukça konik yapılara neden olur ve kat düşüşleri olarak da adlandırılan kat sonlandırma konumları, yüksek tabakalar arası gerilimden kaynaklanan katmanl...
EFFECTS OF THE REACTION MECHANISM ON HEAT RELEASE FOR THE PREDICTION OF THERMOACOUSTIC INSTABILITIES IN LIQUID ROCKET ENGINES
Öztürkmen, Musa Onur; Özyörük, Yusuf (2023-09-13)
NUMERICAL INVESTIGATION OF GENERALIZED K-W TURBULENCE MODEL FOR COMPRESSIBLE DUCT FLOWS
YAHŞİ, ÖMER FARUK; Yılmaz, Mehmet H.; Özyörük, Yusuf; Günaydınlıoğlu, Erkan (2023-09-13)
Estimation of wake induced power losses in a large offshore wind farm using actuator disk and les models
Önel, Hüseyin C.; Tuncer, İsmail Hakkı (2023-09-13)
Numerical wind farm simulations are challenging due to the wide range of length and time scales. Actuator models provide a great trade-off between fidelity and computational cost for the simulation of wind turbines r...
ADJOINT-BASED SHAPE OPTIMIZATION FOR A SEMI-SUBMERGED ENGINE INLET
Küçük, Umut Can; Tuncer, İsmail Hakkı (2023-09-13)
In this study, adjoint-based optimization is conducted for increasing the performance of a semi-submerged inlet exposing a large amount of boundary layer ingestion. Flow and adjoint solutions are conducted with the o...
AERODYNAMIC OPTIMIZATION OF INLET DESIGN FOR HIGH BYPASS RATIO TURBOFAN
KAPLAN, YAĞIZ; Özyörük, Yusuf (2023-09-13)
System Identification of E-VTOL Rotor in Vortex Ring State by Viscous Vortex Particle Method
Şenipek, Murat; Okçu, Ilgaz Doğa; Tekinalp, Ozan; Leblebicioğlu, Mehmet Kemal (2023-09-07)
This paper presents a methodology that identifies a state-space rotor inflow model for a 1.5-m radius two bladed eVTOL rotor in descent. Main purpose of the work is to identify a state-space model for an isolated rotor for...
Unsteady aerodynamic modelling of floating offshore wind turbine rotor using a free wake method
Öztürk, İldeniz; Sezer Uzol, Nilay (2023-07-15)
Flow Visualization Around a Cavitating Tip Vortex
Başkan Perçin, Özge; FISCALETTI, DANIELE; ELSINGA, GERRIT; VAN TERWISGA, TOM (2023-07-13)
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