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
Effects of Rotor Rotor Interactions on Aerodynamic Loads for Two Helicopters in Forward Flight
Date
2010-09-09
Author
Tonkal, Ozan Çağrı
Pehlivan, Sercan
Sezer Uzol, Nilay
İşler, Veysi
Metadata
Show full item record
Item Usage Stats
80
views
0
downloads
Cite This
URI
https://hdl.handle.net/11511/83597
Collections
Unverified, Conference / Seminar
Suggestions
OpenMETU
Core
Effects of design parameters on the aeroelastic performance of a cruise missile wing
Ertürk, Burak; Yaman, Yavuz; Department of Aerospace Engineering (2019)
The design of a cruise missile wing is a multidisciplinary work since the wing has to provide enough aerodynamic forces while being structurally safe. Furthermore, the wing needs to satisfy other considerations such as propulsion, weight, flight performance, sizing for launch platform integration and other measures of merit. In order to meet these design requirements and achieve a successful design, several parameters of the wing need to be investigated at various flight conditions. In this thesis, aeroelas...
Effects of Various Design Parameters on the Performance of a Cruise Missile Wing
Yaman, Yavuz (null; 2019-09-18)
The design of a cruise missile wing is a multidisciplinary work because the wing has to provide enough aerodynamic forces while being structurally in safe. Various parameters of the wing are investigated during the design phase in order to meet the design goals and achieve a successful design. In this paper, the effects of different parameters on the lift force and flutter speed of a cruise missile wing are presented. The aerodynamic analyses for predicting the lift force are performed by using FLUENT and t...
Effects of ambient temperature and drive cycle on electric vehicle charging using photovoltaic systems
Gürer, Erim; Yüksel Bediz, Tuğçe; Sustainable Environment and Energy Systems (2019-8)
Global warming and climate change problem can be solved by only decreasing greenhouse gases (GHGs). About 26% of the global GHG emissions are emitted by the transportation sector. Switching from fossil fuel burning vehicles to electric vehicles is one of the most promising solutions. However, 68% of the electricity is generated by using fossil fuels in the world and if a switch to electric vehicles happens without transforming the electricity generation sector, transportation emissions might even increase. ...
Effects of camberwise varying tip injection on loss and wake characteristics of a low pressure turbine blade
Mercan, Bayram; Dogan, Eda; Ostovan, Yashar; Uzol, Oğuz (2015-08-01)
This paper presents the results of an experimental study that investigates the effects of camberwise varying tip injection on the total pressure loss and wake flow characteristics downstream of a row of Low Pressure Turbine (LPT) blades. This injection technique involves spanwise jets at the tip that are issued from a series of holes distributed along the camber line. The injection from each hole is individually and separately controlled using a computer driven solenoid valve and therefore the flow injectio...
Effects of array guided surface waves on radiation characteristics of a finite planar printed dipole array
Aydın Çivi, Hatice Özlem; Pathak, PH (2004-06-26)
The presence of surface waves different from the conventional grounded dielectric substrate surface wave modes, which can be excited on a finite periodic radiating array of printed dipoles, at frequencies for which the spacing between dipoles is typically less than half a wavelength is studied. The effects of such array guided surface waves on the array radiation characteristics are investigated. Techniques to suppress these surface waves are also discussed.
Citation Formats
IEEE
ACM
APA
CHICAGO
MLA
BibTeX
O. Ç. Tonkal, S. Pehlivan, N. Sezer Uzol, and V. İşler, “Effects of Rotor Rotor Interactions on Aerodynamic Loads for Two Helicopters in Forward Flight,” 2010, Accessed: 00, 2021. [Online]. Available: https://hdl.handle.net/11511/83597.