Vortex shedding behind an inclined flat plate hinged with a trailing-edge flap
© 2019 International Symposium on Turbulence and Shear Flow Phenomena, TSFP. All rights reserved. An influence of a moving motion of a trailing-edge flap on the formation of the wake shed behind an inclined flat plate is investigated via the use of direct numerical simulation (DNS). The leading-edge...
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th-cmuir.6653943832-677862020-04-02T15:06:06Z Vortex shedding behind an inclined flat plate hinged with a trailing-edge flap Nonwarit Borvornsareepirom Jiratrakul Tunkeaw Watchapon Rojanaratanangkule Earth and Planetary Sciences Engineering © 2019 International Symposium on Turbulence and Shear Flow Phenomena, TSFP. All rights reserved. An influence of a moving motion of a trailing-edge flap on the formation of the wake shed behind an inclined flat plate is investigated via the use of direct numerical simulation (DNS). The leading-edge plate is fixed at an angle of attack of 20°, while its rear part flaps according to a time-dependent equation. The chord based Reynolds number is 1000, while the freestream Mach number is set to 0.4. The movement of the trailing-edge flap alters the formation of the leading-edge and trailing-edge vortices. This leads to the modification of the evolution of the unsteady vortex shedding and the acoustic field, resulting in a reduction in the aerodynamic forces. 2020-04-02T15:03:51Z 2020-04-02T15:03:51Z 2019-01-01 Conference Proceeding 2-s2.0-85073595260 https://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=85073595260&origin=inward http://cmuir.cmu.ac.th/jspui/handle/6653943832/67786 |
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Earth and Planetary Sciences Engineering Nonwarit Borvornsareepirom Jiratrakul Tunkeaw Watchapon Rojanaratanangkule Vortex shedding behind an inclined flat plate hinged with a trailing-edge flap |
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© 2019 International Symposium on Turbulence and Shear Flow Phenomena, TSFP. All rights reserved. An influence of a moving motion of a trailing-edge flap on the formation of the wake shed behind an inclined flat plate is investigated via the use of direct numerical simulation (DNS). The leading-edge plate is fixed at an angle of attack of 20°, while its rear part flaps according to a time-dependent equation. The chord based Reynolds number is 1000, while the freestream Mach number is set to 0.4. The movement of the trailing-edge flap alters the formation of the leading-edge and trailing-edge vortices. This leads to the modification of the evolution of the unsteady vortex shedding and the acoustic field, resulting in a reduction in the aerodynamic forces. |
format |
Conference Proceeding |
author |
Nonwarit Borvornsareepirom Jiratrakul Tunkeaw Watchapon Rojanaratanangkule |
author_facet |
Nonwarit Borvornsareepirom Jiratrakul Tunkeaw Watchapon Rojanaratanangkule |
author_sort |
Nonwarit Borvornsareepirom |
title |
Vortex shedding behind an inclined flat plate hinged with a trailing-edge flap |
title_short |
Vortex shedding behind an inclined flat plate hinged with a trailing-edge flap |
title_full |
Vortex shedding behind an inclined flat plate hinged with a trailing-edge flap |
title_fullStr |
Vortex shedding behind an inclined flat plate hinged with a trailing-edge flap |
title_full_unstemmed |
Vortex shedding behind an inclined flat plate hinged with a trailing-edge flap |
title_sort |
vortex shedding behind an inclined flat plate hinged with a trailing-edge flap |
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2020 |
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https://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=85073595260&origin=inward http://cmuir.cmu.ac.th/jspui/handle/6653943832/67786 |
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