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Collaborative studies on flow separation control

Collaborative studies on flow separation control
Collaborative studies on flow separation control
This paper presents the wind tunnel test results concerning the effects of deploying steady and synthetic jets on a NACA0015 airfoil and describes the design of a multi-orifice-single-chamber synthetic jet actuator. Three steady jets with different configurations were tested. The orifice diameter, orientation and spacing were the varying parameters. Synthetic jets were deployed through a single row of orifices that were orientated normal to the airfoil surface. A single row of each type was positioned at 30% of chord from the leading edge. These jets exhibited varying degree of control authority over the lift and drag coefficients. The timescales of attachment and separation were estimated for the test cases of angled steady and synthetic jets. In view of controlling the flow separation in a dynamic manner, a multi-orifice-single-chamber actuator with a typical response time smaller than that of the afore-mentioned time scales was designed, fabricated and tested in quiescent condition.
Airfoil, turbulent separation control, characteristic time, normal jet, angled jet, synthetic jet, multi-orifice, piezo-device, pneumatic device
0925-0042
157-166
Siauw, Wei Long
e829a948-2c78-411f-9945-509dba8043a1
Bonnet, Jean Paul
85b2d317-8dac-40bc-af4d-39e4f18a1669
Tensi, Jean
d4b7044a-b002-4628-a858-54f7502d19b6
Seifert, Avi
cd9a7109-e813-46a7-b68a-686e875c38cc
Stalnov, Oksana
6ca7508b-4d32-4e46-9158-ef8f03795ece
Kumar, Vikas
ced3f095-5e0c-4d6d-a9b5-ce3246eac191
Alvi, Farrukh
f14903e8-5c20-47fb-a886-e7bf7bc815c6
Atkinson, Callum
189433b6-1ef7-4566-8c32-82e5f9113cd0
Trevor, Stephen
99f55a28-96f1-4c18-ab88-3ee6521cf010
Gomes, Luis Daniel
f2fafdb2-54dd-4e5b-9af5-14087198ba5e
Siauw, Wei Long
e829a948-2c78-411f-9945-509dba8043a1
Bonnet, Jean Paul
85b2d317-8dac-40bc-af4d-39e4f18a1669
Tensi, Jean
d4b7044a-b002-4628-a858-54f7502d19b6
Seifert, Avi
cd9a7109-e813-46a7-b68a-686e875c38cc
Stalnov, Oksana
6ca7508b-4d32-4e46-9158-ef8f03795ece
Kumar, Vikas
ced3f095-5e0c-4d6d-a9b5-ce3246eac191
Alvi, Farrukh
f14903e8-5c20-47fb-a886-e7bf7bc815c6
Atkinson, Callum
189433b6-1ef7-4566-8c32-82e5f9113cd0
Trevor, Stephen
99f55a28-96f1-4c18-ab88-3ee6521cf010
Gomes, Luis Daniel
f2fafdb2-54dd-4e5b-9af5-14087198ba5e

Siauw, Wei Long, Bonnet, Jean Paul, Tensi, Jean, Seifert, Avi, Stalnov, Oksana, Kumar, Vikas, Alvi, Farrukh, Atkinson, Callum, Trevor, Stephen and Gomes, Luis Daniel (2008) Collaborative studies on flow separation control. [in special issue: IUTAM Symposium on Flow Control and MEMS - Proceedings of the IUTAM Symposium 2006] Solid Mechanics and Its Applications, 7 (3), 157-166. (doi:10.1007/978-1-4020-6858-4_18).

Record type: Article

Abstract

This paper presents the wind tunnel test results concerning the effects of deploying steady and synthetic jets on a NACA0015 airfoil and describes the design of a multi-orifice-single-chamber synthetic jet actuator. Three steady jets with different configurations were tested. The orifice diameter, orientation and spacing were the varying parameters. Synthetic jets were deployed through a single row of orifices that were orientated normal to the airfoil surface. A single row of each type was positioned at 30% of chord from the leading edge. These jets exhibited varying degree of control authority over the lift and drag coefficients. The timescales of attachment and separation were estimated for the test cases of angled steady and synthetic jets. In view of controlling the flow separation in a dynamic manner, a multi-orifice-single-chamber actuator with a typical response time smaller than that of the afore-mentioned time scales was designed, fabricated and tested in quiescent condition.

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More information

Published date: 2008
Additional Information: ISBN 9781402068577 (print); ISBN 9781402068584 (electronic)
Keywords: Airfoil, turbulent separation control, characteristic time, normal jet, angled jet, synthetic jet, multi-orifice, piezo-device, pneumatic device
Organisations: Aeronautics, Astronautics & Comp. Eng

Identifiers

Local EPrints ID: 344209
URI: http://eprints.soton.ac.uk/id/eprint/344209
ISSN: 0925-0042
PURE UUID: babb559f-c8dc-45c3-887f-f1bacabd767e

Catalogue record

Date deposited: 15 Oct 2012 13:00
Last modified: 14 Mar 2024 12:11

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Contributors

Author: Wei Long Siauw
Author: Jean Paul Bonnet
Author: Jean Tensi
Author: Avi Seifert
Author: Oksana Stalnov
Author: Vikas Kumar
Author: Farrukh Alvi
Author: Callum Atkinson
Author: Stephen Trevor
Author: Luis Daniel Gomes

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