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
Force measurement and load estimation studies at ITU for flexible flapping wings and maneuvering wings under gust
Date
2016-10-25
Author
Son, Onur
Zaloglu, Berk
Perçin, Mustafa
Çetiner Yıldırım, Nuriye Leman Okşan
Metadata
Show full item record
Item Usage Stats
112
views
0
downloads
Cite This
URI
https://hdl.handle.net/11511/72092
Collections
Unverified, Conference / Seminar
Suggestions
OpenMETU
Core
Force generation and wing deformation characteristics of the ’DelFly II’ MAV in hovering flight conditions
Perçin, Mustafa; Remes, Bart (null; 2015-09-15)
Force generation and wing deformation characteristics of a flapping-wing micro air vehicle 'DelFly II' in hovering flight
Perçin, Mustafa; de Croon, G. C. H. E.; Remes, B. (IOP Publishing, 2016-06-01)
The study investigates the aerodynamic performance and the relation between wing deformation and unsteady force generation of a flapping-wing micro air vehicle in hovering flight configuration. Different experiments were performed where fluid forces were acquired with a force sensor, while the three-dimensional wing deformation was measured with a stereo-vision system. In these measurements, time-resolved power consumption and flapping-wing kinematics were also obtained under both in-air and in-vacuum condi...
Force and flowfield measurements of a bio-inspired flapping MAV ‘Delfly Micro’
Deng, Shuanghou; Perçin, Mustafa; van Oudheusden, Bas W.; Remes, Bart; Tenaglia, Andrea (2014-06-18)
Force and motion trajectory tracking control of flexible joint robots
Ider, SK (2000-03-01)
An inverse dynamics control algorithm for constrained flexible-joint robots is developed. It is shown that in a flexible-joint robot, the acceleration level inverse dynamic equations are singular because the control torques do not have an instantaneous effect on the end-effector contact forces and accelerations, due to the elastic media. Implicit numerical integration methods that account for the higher order derivative information are utilized for solving the singular set of differential equations. Joint s...
Drag Analysis of a Supersonic Fighter Aircraft
Akgün, Osman; Golcuk, Ali İhsan; Kurtuluş, Dilek Funda; Kaynak, Ünver (null; 2016-07-15)
For aircraft design, drag optimization is very important for having better flight performance and less fuel consumption. In this study, drag effects of fuselage, wing and tail section are separately analyzed using a generic F-16 fighter aircraft model in ANSYS Fluent CFD tool with polyhedral mesh. Pressure drag and viscous drag effects are shown on different section of the aircraft as fuselage, wing, vertical tail and horizontal tail. Drag values are presented on subsonic, transonic and supersonic flights.
Citation Formats
IEEE
ACM
APA
CHICAGO
MLA
BibTeX
O. Son, B. Zaloglu, M. Perçin, and N. L. O. Çetiner Yıldırım, “Force measurement and load estimation studies at ITU for flexible flapping wings and maneuvering wings under gust,” 2016, Accessed: 00, 2021. [Online]. Available: https://hdl.handle.net/11511/72092.