Active Flow Control on Vertical Tail Models
نویسندگان
چکیده
منابع مشابه
Active Vertical Tail Buffeting Alleviation on a Twin-tail Fighter Configuration in a Wind Tunnel
A 1/6-scale F-18 wind-tunnel model was tested in the Transonic Dynamics Tunnel at the NASA Langley Research Center as part of the Actively Controlled Response Of Buffet-Affected Tails (ACROBAT) program to assess the use of active controls in reducing vertical tail buffeting. The starboard vertical tail was equipped with an active rudder and other aerodynamic devices, and the port vertical tail ...
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This Article is brought to you for free and open access by the Engineering Technology at ODU Digital Commons. It has been accepted for inclusion in Engineering Technology Faculty Publications by an authorized administrator of ODU Digital Commons. For more information, please contact [email protected]. Repository Citation Jun, Wang; Shaoping, Wang; Xingjian, Wang; Cun, Shi; and Tomovic, Mil...
متن کاملExperimental Investigation of the Effect of Vertical Tail on the Flow Field and Aerodynamic Forces of a fighter Model
An intensive experimental investigation was conducted to study the effect of vertical tail, single and twin (with different cant angles) on the flow field and the corresponding aerodynamic forces and moments of a model of a fighter A/C. Aerodynamic forces under different flight conditions and different vertical tail settings were measured in a supersonic wind tunnel. Furthermore, effects of ver...
متن کاملExperimental Investigation of the Effect of Vertical Tail on the Flow Field and Aerodynamic Forces of a fighter Model
An intensive experimental investigation was conducted to study the effect of vertical tail, single and twin (with different cant angles) on the flow field and the corresponding aerodynamic forces and moments of a model of a fighter A/C. Aerodynamic forces under different flight conditions and different vertical tail settings were measured in a supersonic wind tunnel. Furthermore, effects of ver...
متن کاملActive Vertical Tail Buffeting Alleviation on an F/a-18 Model in a Wind Tunnel
A 1/6-scale F-18 wind-tunnel model was tested in the Transonic Dynamics Tunnel at the NASA Langley Research Center as part of the Actively Controlled Response Of Buffet-Affected Tails (ACROBAT) program to assess the use of active controls in reducing vertical tail buffeting. The starboard vertical tail was equipped with an active rudder and other aerodynamic devices, and the port vertical tail ...
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ژورنال
عنوان ژورنال: AIAA Journal
سال: 2019
ISSN: 0001-1452,1533-385X
DOI: 10.2514/1.j057876