Yıl: 2020 Cilt: 40 Sayı: 1 Sayfa Aralığı: 131 - 139 Metin Dili: İngilizce İndeks Tarihi: 17-10-2020

INVESTIGATING THE EFFECTS OF PLASMA ACTUATOR ON THE FLOW CONTROL AROUND NACA2415 AIRFOIL

Öz:
In this study, the effects of the plasma actuator on flow control at varied Reynolds numbers and attack angles are examined. Plasma actuator is placed on the NACA2415 airfoil at x/C = 0.1. The effect of the actuator to active flow control is examined at Reynolds number between 8x103and 9x104in the wind tunnel. The lift force which acted on the airfoil was measured by using a force balance system. The velocity measurements were done by the hot-wire probe, located at the wake region, and the flow around model was visualized by the smoke wire method. When the plasma was active, an increased lift force and a narrowed wake region are observed. The stall angle shifted to the higher attack angle by the effective active flow control at low Reynolds numbers. Prevent of the flow separation was enhanced up to 18° angle of attack and the maximum lift force occurred at the 14° angle of attack which is doubled when the plasma actuator is on.
Anahtar Kelime:

Belge Türü: Makale Makale Türü: Araştırma Makalesi Erişim Türü: Erişime Açık
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APA ŞANLISOY A, AKANSU Y (2020). INVESTIGATING THE EFFECTS OF PLASMA ACTUATOR ON THE FLOW CONTROL AROUND NACA2415 AIRFOIL. , 131 - 139.
Chicago ŞANLISOY Aytaç,AKANSU Yahya Erkan INVESTIGATING THE EFFECTS OF PLASMA ACTUATOR ON THE FLOW CONTROL AROUND NACA2415 AIRFOIL. (2020): 131 - 139.
MLA ŞANLISOY Aytaç,AKANSU Yahya Erkan INVESTIGATING THE EFFECTS OF PLASMA ACTUATOR ON THE FLOW CONTROL AROUND NACA2415 AIRFOIL. , 2020, ss.131 - 139.
AMA ŞANLISOY A,AKANSU Y INVESTIGATING THE EFFECTS OF PLASMA ACTUATOR ON THE FLOW CONTROL AROUND NACA2415 AIRFOIL. . 2020; 131 - 139.
Vancouver ŞANLISOY A,AKANSU Y INVESTIGATING THE EFFECTS OF PLASMA ACTUATOR ON THE FLOW CONTROL AROUND NACA2415 AIRFOIL. . 2020; 131 - 139.
IEEE ŞANLISOY A,AKANSU Y "INVESTIGATING THE EFFECTS OF PLASMA ACTUATOR ON THE FLOW CONTROL AROUND NACA2415 AIRFOIL." , ss.131 - 139, 2020.
ISNAD ŞANLISOY, Aytaç - AKANSU, Yahya Erkan. "INVESTIGATING THE EFFECTS OF PLASMA ACTUATOR ON THE FLOW CONTROL AROUND NACA2415 AIRFOIL". (2020), 131-139.
APA ŞANLISOY A, AKANSU Y (2020). INVESTIGATING THE EFFECTS OF PLASMA ACTUATOR ON THE FLOW CONTROL AROUND NACA2415 AIRFOIL. Isı Bilimi ve Tekniği Dergisi, 40(1), 131 - 139.
Chicago ŞANLISOY Aytaç,AKANSU Yahya Erkan INVESTIGATING THE EFFECTS OF PLASMA ACTUATOR ON THE FLOW CONTROL AROUND NACA2415 AIRFOIL. Isı Bilimi ve Tekniği Dergisi 40, no.1 (2020): 131 - 139.
MLA ŞANLISOY Aytaç,AKANSU Yahya Erkan INVESTIGATING THE EFFECTS OF PLASMA ACTUATOR ON THE FLOW CONTROL AROUND NACA2415 AIRFOIL. Isı Bilimi ve Tekniği Dergisi, vol.40, no.1, 2020, ss.131 - 139.
AMA ŞANLISOY A,AKANSU Y INVESTIGATING THE EFFECTS OF PLASMA ACTUATOR ON THE FLOW CONTROL AROUND NACA2415 AIRFOIL. Isı Bilimi ve Tekniği Dergisi. 2020; 40(1): 131 - 139.
Vancouver ŞANLISOY A,AKANSU Y INVESTIGATING THE EFFECTS OF PLASMA ACTUATOR ON THE FLOW CONTROL AROUND NACA2415 AIRFOIL. Isı Bilimi ve Tekniği Dergisi. 2020; 40(1): 131 - 139.
IEEE ŞANLISOY A,AKANSU Y "INVESTIGATING THE EFFECTS OF PLASMA ACTUATOR ON THE FLOW CONTROL AROUND NACA2415 AIRFOIL." Isı Bilimi ve Tekniği Dergisi, 40, ss.131 - 139, 2020.
ISNAD ŞANLISOY, Aytaç - AKANSU, Yahya Erkan. "INVESTIGATING THE EFFECTS OF PLASMA ACTUATOR ON THE FLOW CONTROL AROUND NACA2415 AIRFOIL". Isı Bilimi ve Tekniği Dergisi 40/1 (2020), 131-139.