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Effect of Wing Heating of Flow Structure of Low Swept Delta Wing
Date
2017-09-22
Author
Şencan, Gizem
Güvenç Yazıcıoğlu, Almıla
Yavuz, Mehmet Metin
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URI
https://hdl.handle.net/11511/78607
Conference Name
9th. Ankara International Aerospace Conference, 2017
Collections
Department of Mechanical Engineering, Conference / Seminar
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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 Edge Modifications on Flow Structure of Low Swept Delta Wing
Celik, Alper; Yavuz, Mehmet Metin (2016-05-01)
Effect of ground on flow structure of non-slender delta and reverse delta wings
Koçak, Göktuğ; Yavuz, Mehmet Metin; Department of Mechanical Engineering (2023-1-26)
Flight condition of aircrafts proximity to the ground, so-called “Ground Effect” (GE), is among one of the most recent research areas since the aerodynamic performance and stability of wing in ground effect (WIG) crafts significantly vary due to the flow dynamics associated with the interaction between the wing and the surface. In the present study, ground effect of non-slender delta wings (DW) and reversed delta wings (RDW) at static ground effect (SGE) condition in the absence of heave and pitch motion w...
Effect of forward velocity on rectangular wings flapping with piezoelectric actuators
Çömez, Fadile Yudum; Kurtuluş, Dilek Funda (null; 2018-07-11)
In the current study, unsteady aerodynamic forces of two flapping rectangular wings are investigated using two different materials namely, aluminum and plexigla ss. Two different materials used for the wings are intended to observe the effects of the wing flexibility on instantaneous aerodynamic forces. A Lead Zirconate Titanate (PZT) piezoelectric actuator is used for flapping the wing models. The wind tunnel tests are performed with velocities ranging from 0m/s to 12 m/s. Output flapping frequencies are m...
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G. Şencan, A. Güvenç Yazıcıoğlu, and M. M. Yavuz, “Effect of Wing Heating of Flow Structure of Low Swept Delta Wing,” presented at the 9th. Ankara International Aerospace Conference, 2017, Ankara, Türkiye, 2017, Accessed: 00, 2021. [Online]. Available: https://hdl.handle.net/11511/78607.