Bir inşaat sahasinda mevcut şevlerin performans değerlendirmesi ve önlem odakli kesin tasarimi

Yunatçı, Ali Anıl
Bilge, Habib Tolga
Çetin, Kemal Önder
Zemin Mekanigi ve Temel Muhendisligi 15. Ulusal Kongresi


Improvement of finite element model by using sine vibration test results of acommunication satellite
Çekiç, Abdulkadir; Yaman, Yavuz; Department of Aerospace Engineering (2021-2-15)
In this thesis, the vibration analysis of a communication satellite is performed,and the improvementof the finite element model by using vibration test results is presented. First, the satellite finite element model isgenerated using MSC/PATRAN and MSC/NASTRAN commercial software. With the natural frequency and frequency response analysis, the expected frequency values and response amplitudes in accelerometers arecalculated in vibration tests. The results obtained in the vib...
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Evaluation of best environmental management practices of an integrated iron and steel plant
Çakır, Nur; Yetiş, Ülkü; Alp, Emre; Department of Environmental Engineering (2012)
European Union published IPPC Directive in 1996 aiming to create an integrated approach in order to manage and control industrial facilities better. IPPC provides the development of a new concept of “Best Available Techniques (BAT)”, the most effective, advanced and applicable methods, preventing emissions to the environment and providing efficient use of resources. Within this framework, numerous sectoral Best Available Techniques Reference Documents were published giving information on the sector and BAT ...
Determination of loads on a flexible wing of a fighter jet via surrogate models
Zafer, Özgür; Şahin, Melin; Department of Aerospace Engineering (2023-1-26)
This study presents the load analysis of a flexible wing for a fighter jet. The main purpose is to demonstrate the application of a rapid methodology for aero-structural coupling and the determination of flexible wing loads suitable for the initial design stages of a fighter jet. The present methodology allows designers to include flexibility effects early on and to explore the design space quickly for flexible wing loads. The methodology uses an aerodynamic database obtained with high-fidelity computationa...
Multidisciplinary design and optimization of a composite wing box
Hasan, Muvaffak; Yaman, Yavuz; Department of Aerospace Engineering (2003)
In this study an automated multidisciplinary design optimization code is developed for the minimum weight design of a composite wing box. The multidisciplinary static strength, aeroelastic stability, and manufacturing requirements are simultaneously addressed in a global optimization environment through a genetic search algorithm. The static strength requirements include obtaining positive margins of safety for all the structural parts. The modified engineering bending theory together with the coarse finite...
Citation Formats
A. A. Yunatçı, H. T. Bilge, and K. Ö. Çetin, “Bir inşaat sahasinda mevcut şevlerin performans değerlendirmesi ve önlem odakli kesin tasarimi,” presented at the Zemin Mekanigi ve Temel Muhendisligi 15. Ulusal Kongresi, Ankara, Türkiye, 2014, Accessed: 00, 2021. [Online]. Available: