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Effect of Edge Modifications on Flow Structure of Low Swept Delta Wing
Date
2016-05-01
Author
Celik, Alper
Yavuz, Mehmet Metin
Metadata
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Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License
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URI
https://hdl.handle.net/11511/46733
Journal
AIAA JOURNAL
DOI
https://doi.org/10.2514/1.j054587
Collections
Department of Mechanical Engineering, Article
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Effect of wing heating on flow structure of low swept delta wing
Şencan, Gizem; Yavuz, Mehmet Metin; Güvenç Yazıcıoğlu, Almıla; Department of Mechanical Engineering (2016)
Micro Air Vehicles (MAVs), Unmanned Air Vehicles (UAVs) and Unmanned Combat Air Vehicles (UCAVs), which can be represented by simplified planforms including low swept delta wings, have many advantages in defense industry and aeronautical field. Thus, the aerodynamics of nonslender delta wings including development and application of different flow control techniques have been of considerable interest in recent years. In this study, it is aimed to investigate the effect of heating on the flow structure over...
Effect of blowing pattern through leading edge on flow structure of 45 degree swept delta wing
Günacar, Gökay; Yavuz, Mehmet Metin; Department of Mechanical Engineering (2016)
There has been an increasing interest in recent years in control of flow structure over non-slender delta wings, which are the simplified planforms of Unmanned Air Vehicles (UAV), Unmanned Combat Air Vehicles (UCAV), and Micro Air Vehicles (MAV). Different control approaches have been applied to alter the flow structure with particular interests in preventing stall and delaying vortex breakdown. Among different flow control techniques, blowing through leading edge of the wing has been commonly used due to i...
Effect of Wing Heating of Flow Structure of Low Swept Delta Wing
Şencan, Gizem; Güvenç Yazıcıoğlu, Almıla; Yavuz, Mehmet Metin (null; 2017-09-22)
Effect of bleed opening ratio on flow structure of a nonslender delta wing
Kestel, Kayaca; Yavuz, M. Metin,; Department of Mechanical Engineering (2019)
Boundaries of the aircraft industry need to expand since both economic and ecologic constraints are getting more challenging. The usage of Unmanned Air Vehicles(UAV), Unmanned Combat Air Vehicles(UCAV), and Micro Air Vehicles(MAV) which can be simplified as non-slender delta wing plan-forms has been increasing during the last few decades, primarily due to their superiority over commercial airplanes. Hence, researchers have aimed to control the complex flow structures on non-slender delta wings with particul...
Effect of Thickness-to-Chord Ratio on Flow Structure of a Low Swept Delta Wing
Gulsacan, Burak; Sencan, Gizem; Yavuz, Mehmet Metin (American Institute of Aeronautics and Astronautics (AIAA), 2018-12-01)
The effect of thickness-to-chord (t/C) ratio on flow structure of a delta wing with sweep angle of 35 deg is characterized in a low-speed wind tunnel using laser-illuminated smoke visualization, particle image velocimetry, and surface pressure measurements. Four different t/C ratios varying from 4.75 to 19% are tested at angles of attack, 4, 6, 8, and 10 deg, for Reynolds numbers Re =1 x 10(4) and 3.5 x 10(4). The results indicate that the effect of thicknessto-chord ratio on flow structure is quite substan...
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A. Celik and M. M. Yavuz, “Effect of Edge Modifications on Flow Structure of Low Swept Delta Wing,”
AIAA JOURNAL
, pp. 1789–1797, 2016, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/46733.