Gevşek Bağlı Bir Akışkan Katı Etkileşimi Yöntemi Kullanılarak Narin Bir Füzenin Statik Aeroelastik Analizlerinin Yapılması

Date

2012-09-12

Author

Akgül, Mehmet
Akgül, Ali
Sert, Cüneyt

Metadata

Show full item record

This work is licensed under a Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.

Item Usage Stats

118
views

0
downloads

URI

https://hdl.handle.net/11511/89098

Collections

Department of Mechanical Engineering, Conference / Seminar

Suggestions

OpenMETU
Core

Static aeroelastic analysis of a generic slender missile using a loosely coupled fluid structure interaction method Akgül, Mehmet; Sert, Cüneyt; Department of Mechanical Engineering (2012) There are many active and passive vibration control techniques to reduce the effect of energy on structures which emerges during an earthquake and reduce the displacement of buildings that is caused by ground acceleration. Main advantage of passive vibration control techniques over active vibration control techniques is; no external power or a sensor is required for passive vibration control devices (PVCDs) and it results in lower installation and maintenance costs. However, PVCDs require a predefined optim...
Comparison of EKF, EKF2 and UKF in a loosely coupled INS/GPS integration Jane, Hande; Baykal, Buyurman; Department of Electrical and Electronics Engineering (2018) Developing effective navigation solutions in land, sea, air, and space travels is an ever increasing necessity maintaining its validity. Nowadays, although a navigation aid called satellite based Global Positioning System (GPS) is used to develop a navigation solution, standalone GPS cannot achieve the desired accuracy in some applications. For this reason, GPS measurements are integrated with the Inertial Navigation System (INS) to develop an enhanced accurate integrated navigation solution. Extended Kalma...
Aeroelastic analysis of composite wings and wind turbine blades including geometrical nonlinearity and compressibilty Farsadi, Touraj; Kayran, Altan; Department of Aerospace Engineering (2018) Aeroelastic behaviour of composite wings and wind turbine blades in the incompressible and compressible flow regimes is investigated utilizing a geometrically nonlinear Thin Wall Beam (TWB) theory incorporating non uniform geometric features such as sweep, taper, pretwist, warping inhibition and transverse shear strain. The structural equations of motion are obtained in the most general form based on the kinematic relations governing thin walled beams, including the nonlinear strain displacement relations, ...
Failure analysis of tapered composite structures under tensile loading Çelik, Ozan; Parnas, Kemal Levend; Department of Mechanical Engineering (2016) A three dimensional finite element modeling approach is used to evaluate the effects of preliminary design variables on the performance of tapered composite laminates under tensile loading. Hashin failure criteria combined with a progressive failure algorithm is used for in-plane failure mechanisms and cohesive zone method is used for out-of-plane failures. The modeling approach is validated by a comparison with experimental results from literature. The validated model is used to examine various design vari...
Investigation of buckling, post-buckling behaviour of variable stiffness composite plates Cömert, Utku Kaan; Darendeliler, Haluk; Department of Mechanical Engineering (2022-8-31) In this thesis, buckling and post-buckling behaviour of variable stiffness (VS) composite plates are investigated. VS plates are designed by using quadratic Bezier curves to define fiber paths and a script is written for this purpose. Manufacturing limitations and defects are included into the simulations. In the analyses, Finite Element Method (FEM) is used to solve linear and nonlinear buckling with Hashin failure criterion. The plates constructed by using fiber paths with linear and nonlinear angle varia...

Citation Formats

M. Akgül, A. Akgül, and C. Sert, “Gevşek Bağlı Bir Akışkan Katı Etkileşimi Yöntemi Kullanılarak Narin Bir Füzenin Statik Aeroelastik Analizlerinin Yapılması,” 2012, Accessed: 00, 2021. [Online]. Available: https://hdl.handle.net/11511/89098.