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
Aeroelastic analyses and tests of a wing like structure with payload
Download
index.pdf
Date
2019
Author
Serin, Özgür
Metadata
Show full item record
This work is licensed under a
Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License
.
Item Usage Stats
340
views
147
downloads
Cite This
In this study, a wing-like structure with three payloads was examined from the point of flutter characteristic by performing frequency domain flutter analyses in a commercial software ZAERO© and conducting wind tunnel flutter tests in Ankara Wind Tunnel (ART) test facility. Based upon the aeroelastic certification flow admitted by the independent aviation authorities being active across the globe, for each configuration of the wing-like structure, finite element models were created using Altair Hypermesh© software, finite element modal analyses were realized with the solver of MSC Nastran© and ground vibration tests were conducted with Simcenter Scadas© data acquisition system. For the purpose of obtaining more accurate flutter analysis results, required finite element models of the configurations were modal updated per the ground vibration test results. Afterwards, the flutter onset speeds and frequencies for each configuration were acquired with the flutter analyses realized by applying the finite element modal analysis results of both updated and non-updated finite element models. All these outputs were compared with the flutter onset speeds and frequencies ascertained in the wind tunnel tests and consistency between the analysis and the test was investigated. In addition, the influence of the installation of three payloads to the wing-like structure in different combinations was studied in the sense of flutter behavior and the reasons of unexpected results were interpreted by further analysis and tests.
Subject Keywords
Payloads (Aerospace engineering).
,
Keywords: Aeroelasticity
,
Flutter Analysis
,
Ground Vibration Test
,
Modal Updating
,
Wind Tunnel Flutter Test.
URI
http://etd.lib.metu.edu.tr/upload/12623459/index.pdf
https://hdl.handle.net/11511/43589
Collections
Graduate School of Natural and Applied Sciences, Thesis
Suggestions
OpenMETU
Core
Flutter characteristics of plate like structures
Dalmış, Mevlüt Burak; Yazıcıoğlu, Yiğit; Durak, Burak; Department of Mechanical Engineering (2014)
In this study, flutter characteristics of plate like structures in incompressible flow are investigated by comparing the results of commercial flutter analysis program ZAERO© with wind tunnel tests conducted in Ankara Wind Tunnel (ART). Firstly, a rectangular polycarbonate (PC) plate, 5x125x1000 mm in dimensions, is investigated. In this case, analysis and test results are in good agreement with each other. Second test item is a 1/10 scaled F-16 wing like PC plate. In this case, the plate is capable of carr...
Atmospheric boundary layer simulation in a short wind tunnel
Shojaee, S. M. N.; Uzol, Oğuz; Kurç, Özgür (2014-02-01)
This paper presents the design, computational analysis and experimental study of passive device configurations which utilized in the Ankara Wind Tunnel to simulate the atmospheric boundary layer within the test section. The study here is part of a joint project between the Aerospace and Civil Engineering Departments at Middle East Technical University, which involves testing of high-rise building models in the Ankara Wind Tunnel. The design consists of spires and rows of cubical surface roughness elements a...
Aerodynamic optimization of turbomachinery cascades using Euler/boundary-layer coupled genetic algorithms
Oksuz, O; Akmandor, IS; Kavsaoglu, MS (American Institute of Aeronautics and Astronautics (AIAA), 2002-05-01)
A new methodology is developed to find the optimal aerodynamic performance of a turbine cascade. A boundary-layer coupled Euler algorithm and a genetic algorithm are linked within an automated optimization loop. The multiparameter objective function is based on the blade loading. For a given inlet Mach number and baseline cascade geometry, the flow inlet and exit angles, the blade thickness and the solidity are optimized by a robust genetic algorithm. First, the Sanz subcritical turbine cascade is selected ...
Flow Structure on Nonslender Delta Wing: Reynolds Number Dependence and Flow Control
Zharfa, Mohammadreza; Ozturk, Ilhan; Yavuz, Mehmet Metin (2016-03-01)
The flow structure over a 35 deg swept delta wing is characterized in a low-speed wind tunnel using techniques of laser-illuminated smoke visualization, laser Doppler anemometry, and surface-pressure measurements. The effects of Reynolds numbers and attack angles on the evaluation of flow patterns are addressed within the broad range of Reynolds number 10(4) < Re < 10(5) and attack angle 3 deg < alpha < 10 deg. In addition, the effect of steady blowing through the leading edges of the wing on flow structure...
Experimental analysis of flow structure on moderate sweep delta wing
Öztürk, İlhan; Yavuz, Mehmet Metin; Department of Mechanical Engineering (2014)
Experimental investigation of flow over a 45° moderate swept delta wing is performed using laser illuminated smoke visualization, surface pressure measurements, and Laser Doppler Anemometry (LDA) techniques in low-speed wind tunnel. The formation of leading-edge vortices and their breakdown, and three-dimensional separation from the surface of the wing are studied at broad range of attack angles and Reynolds numbers. Smoke visualizations are performed at three different cross flow planes along with vortex a...
Citation Formats
IEEE
ACM
APA
CHICAGO
MLA
BibTeX
Ö. Serin, “Aeroelastic analyses and tests of a wing like structure with payload,” Thesis (M.S.) -- Graduate School of Natural and Applied Sciences. Aerospace Engineering., Middle East Technical University, 2019.