Show/Hide Menu
Hide/Show Apps
Logout
Türkçe
Türkçe
Search
Search
Login
Login
OpenMETU
OpenMETU
About
About
Open Science Policy
Open Science Policy
Open Access Guideline
Open Access Guideline
Postgraduate Thesis Guideline
Postgraduate Thesis Guideline
Communities & Collections
Communities & Collections
Help
Help
Frequently Asked Questions
Frequently Asked Questions
Guides
Guides
Thesis submission
Thesis submission
MS without thesis term project submission
MS without thesis term project submission
Publication submission with DOI
Publication submission with DOI
Publication submission
Publication submission
Supporting Information
Supporting Information
General Information
General Information
Copyright, Embargo and License
Copyright, Embargo and License
Contact us
Contact us
High strain rate material characterization of Al 7075-T651 by modified Taylor impact test and velocity interferometry
Date
2017-01-01
Author
Kesemen, Latif
Kayran, Altan
Metadata
Show full item record
This work is licensed under a
Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License
.
Item Usage Stats
195
views
0
downloads
Cite This
© 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.Metallic materials in aerospace structures are exposed to impact loading depending on their usage area. High strain rate material characterization of metallic materials is very crucial to properly prepare finite element models to be used in impact loading situations. Aluminum alloys are widely used in aerospace structures in variety of areas. Johnson-Cook material model is a suitable material model to represent the behaviour of aluminum alloys at high strain rates. In the present study, parameters of the Johnson-Cook yield strength model for the Al 7075-T651 material are determined utilizing the combination of the quasi-static tensile test and the modified Taylor impact test. High strain rate material characterization of Al 7075-T651 is performed by the modified Taylor impact test and velocity interferometry. Modified Taylor impact test system and how the free surface velocity measurement by the velocity interferometry is utilized for the determination of the yield strength and the strain rate constant of the Johnson-Cook yield strength model are described in detail. Experimentally determined parameters of the Johnson-Cook model are used in Autodyn simulation of the modified Taylor impact test. Experimentally and numerically determined free surface velocities are compared and reasonably good agreement is obtained between the test and simulation results with a small offset between the velocity profiles.
URI
https://hdl.handle.net/11511/56120
DOI
https://doi.org/10.2514/6.2017-0354
Collections
Department of Aerospace Engineering, Conference / Seminar
Suggestions
OpenMETU
Core
Adaptive roll control of guided munitions with state independent uncertainty parameterization
Ovec, Naz T.; Kutay, Ali Türker (2017-01-01)
© 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.Guided munitions are air-to-air or air-to-surface weapons which have enhanced target hit capabilities with laser seekers or similar guidance utilities. The additional components enhance the target hit capability of the munition significantly but they bring along some aerodynamic challenges as well. The cross-coupled interactions are triggered with the sharp maneuvers and the stabilization of the roll channel is aggrava...
Modification of the extended messinger model for mixed phase icing and industrial applications with TAICE
Ayan, Erdem; Özgen, Serkan (2017-01-01)
© 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.Computational studies have been performed in order to predict mixed phase ice accretion on aircraft components. In-house developed TAICE tool has been used in this study. Previously, TAICE was already validated for icing cases due to water droplets only. In addition, in the framework of High Altitude Ice Crystals (HAIC) FP7 European project, mixed phase ice accretion prediction capability has been added to TAICE. Up to...
Adaptive model predictive control of uncertain systems with input constraints
Yayla, Metehan; Kutay, Ali Türker (2017-01-01)
© 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.This paper introduces a new hybrid adaptive model predictive control approach to control of uncertain dynamical systems where the matched uncertainty can be linearly parameterized by known basis functions. Introduced control framework respects the actuator position limit and actuator rate limit. Initially, an integration method in adaptive control is employed to identify the matched uncertainty in conjunction with Pseu...
Analysis of effects of different diffusion models in hypersonic flow regimes
Gur, H. Berk; Eyi, Sinan (2017-01-01)
© 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.Hypersonic flows become popular due to its use in space explorations and military applications. It occurs normally, when a space craft re-enter to the atmosphere. Space crafts are exposed to high temperatures and high pressures because of Earth’s atmosphere and gravity. In addition in high temperatures, gases tend to react with each other. These reactions also have effects on space craft’s surface. In order to calculat...
Fully transient conjugate analysis of silica-phenolic charing ablation coupled with interior ballistics
Alanyalıoğlu, Çetin Ozan; Özyörük, Yusuf (2019-01-01)
© 2019, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.Due to its excellent insulation capability, usage of silica-phenolic charring ablator as nozzle liner is a common practice in solid rocket motor industry. During the design of a solid rocket motor employing silica-phenolic as nozzle liner, it is desired to conduct an accurate analysis yielding in-depth thermal response and recession characteristics. As the interior ballistics and nozzle recession rate mutually interact...
Citation Formats
IEEE
ACM
APA
CHICAGO
MLA
BibTeX
L. Kesemen and A. Kayran, “High strain rate material characterization of Al 7075-T651 by modified Taylor impact test and velocity interferometry,” 2017, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/56120.