Development of a Wing Preliminary Struıctural Analysis Code

2002-01-01
Yaman, Yavuz
Show full item record
51
views
0
downloads
https://hdl.handle.net/11511/82274
Journal of Aircraft
Unverified, Article

Suggestions

Development of a Wing Preliminary Structural Analysis code
Yaman, Yavuz (American Institute of Aeronautics and Astronautics (AIAA), 2002-05-01)
Design of a grid fin aerodynamic control device for transonic flight regime
Dikbaş, Erdem; Sert, Cüneyt; Baran, Özgür Uğraş; Department of Mechanical Engineering (2015)
Grid fins is unconventional control devices and they are used for aerodynamic control of various types of missiles. Low hinge moment requirement and superior packaging possibilities make grid fins attractive when compared to conventional planar fins. However, design of grid fins is more involved when transonic flight regime is considered. The reason for this is high drag force encountered by the grid fin. The purpose of the thesis is to overcome this drawback and to define a proper design methodology for tr...
DEVELOPMENT OF A 3-D TOPOGRAPHICAL BASIN STRUCTURE BASED ON SEISMIC AND GEOTECHNICAL DATA: CASE STUDY AT A HIGH SEISMICTY AREA OF GÖLYAKA, DÜZCE, TURKEY
Yousefıbavıl, Karim; Koçkar, Mustafa Kerem; Akgün, Haluk (2018-06-21)
The near-fault situation and high seismicity of an area makes the determination of the bedrock geometry more complex, and in return, it makes this area much more critical and important for the studies of site response analysis in account of seismic hazard assessment. Without a good model of topography and basin structure, any powerful calculation method would be in lack of a well-developed basin response. The study has been conducted in the Gölyaka basin that uniquely falls within the bifurcated section of ...
Design and investigation of a new type rotary vane air compresser and expander
Okutur, A. Selim; Göksel, Ömer; Department of Mechanical Engineering (1984)
Development of a UAV testbed
Çakır, Zeynep; Yavrucuk, İlkay; Tekinalp, Ozan; Department of Aerospace Engineering (2011)
The development and testing for a UAV testbed to be used in academic research and undergraduate education is proposed in this thesis. Analysis on commercial off -the-shelf UAV systems and autopilots lead to the development of a custom, open-architecture and modular UAV testbed. The main focus is to support research in UAV control field and education of the undergraduate students. The integration and use of commercial-off -the-shelf avionics and air vehicle are described in detail. System performance is exam...
Citation Formats
Y. Yaman, “Development of a Wing Preliminary Struıctural Analysis Code,” Journal of Aircraft, pp. 512–514, 2002, Accessed: 00, 2021. [Online]. Available: https://hdl.handle.net/11511/82274.
METU IIS - Integrated Information Service open@metu.edu.tr