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
Morphing Wing Optimization for Steady Level Flight
Date
2015-06-29
Author
Körpe, Durmuş Sinan
Özgen, Serkan
Metadata
Show full item record
Item Usage Stats
55
views
0
downloads
Cite This
URI
https://hdl.handle.net/11511/72675
Collections
Unverified, Conference / Seminar
Suggestions
OpenMETU
Core
Morphing wing optimization for steady level flight
Korpe, Durmus S.; Özgen, Serkan (2017-11-01)
This paper presents the basic results of the morphing wing planform optimization of an experimental unmanned air vehicle for minimum drag at steady level flight. The aerodynamic design tool that consists of the three-dimensional panel method, two-dimensional boundary layer solution and generalized reduced gradient method-based optimization is appropriate for fixed wing and morphing wing conceptual and preliminary design. The morphing concept is implemented into the solution with the geometric constraints of...
Morphing Air Vehicle Concepts
Özgen, Serkan; Yaman, Yavuz; Şahin, Melin; Erdoğan Tolga, İnsuyu; Ünlüsoy, Levent; Bayram, Göknur; Uludağ, Yusuf; Yılmaz, Ayşen (2010-06-10)
This article summarizes the current level and trends in the emerging Morphing Air Vehicle Technology. The worldwide status of the research is introduced together with proposals related to the design and development of such vehicles from aerodynamics, flight mechanics, material sciences, and structures points of view. Part I introduces the morphing concept and its potential. Part II summarizes the present technological level, while Part III discusses technological challenges and solution proposals.
Morphing wings and control surfaces: A new approach in aircraft design
Yaman, Yavuz (2017-07-05)
This paper details the fully morphing wings and control surfaces. The idea of morphing is particularly attractive in aircraft technologies. Various approaches like span increase, camber increase and/or decrease, twist, and sweep are finding extensive applications in aeronautical structures.
Morphing Estimated Human Intention via Human-Robot Interactions
Durdu, Akif; Erkmen, İsmet; Erkmen, Aydan Müşerref; Yilmaz, Alper (2011-10-21)
Estimating and reshaping human intentions are topics of research in the field of human-robot interaction. Although works on estimating human intentions are quite well known research areas in the literature, reshaping intentions through interactions is a new significant branching in the field of human-robot interaction. In this paper, we research how the human intentions change based on his/her actions by moving the robots in a real human-robot environment. Our approach uses the Hidden Markov Model (HMM) tai...
Morphing for motion estimation
Genc, S; Yarman Vural, Fatoş Tunay (1999-07-01)
A new approach is presented for motion estimation and modeling. The proposed method morphs the final frame of a sequence of motion frames from the initial frame. The morphing parameters are estimated using the intermediate frames. The morphing algorithm uses the warping and cross-dissolve techniques used in the recent morphing algorithms. However, rather then using the displacement of line pairs, a set of control points is used. A new method is proposed for the identification of the control points. For this...
Citation Formats
IEEE
ACM
APA
CHICAGO
MLA
BibTeX
D. S. Körpe and S. Özgen, “Morphing Wing Optimization for Steady Level Flight,” 2015, Accessed: 00, 2021. [Online]. Available: https://hdl.handle.net/11511/72675.