Comptes Rendus
Separation flow control
Experimental detection of flow separation over a plain flap by wall shear stress analysis with and without steady blowing
[Détection expérimentale du décollement de l'écoulement sur un volet sans fente par l'analyse du frottement pariétal avec ou sans soufflage continu]
Comptes Rendus. Mécanique, Volume 342 (2014) no. 6-7, pp. 389-402.

Cet article traite de la détection du décollement de l'écoulement sur un volet sans fente pour un nombre de Reynolds de 2106 par l'analyse des fluctuations du frottement pariétal. On considère en premier lieu le décollement naturel à travers l'étude de l'évolution des fluctuations de frottement pariétal mesurées sur la corde du volet lorsque son angle de braquage augmente progressivement. Par la suite, un contrôle par soufflage continu est appliqué et l'effet de ce contrôle sur les fluctuations de frottement pariétal est étudié. Dans les cas contrôlé et non contrôlé, des critères de décollement sont définis, étudiés et comparés entre eux.

The present article deals with the flow separation detection over a plain flap at a Reynolds number of 2106 by the analysis of the wall shear stress fluctuations. Natural flow separation is first considered with the study of the evolution of wall shear stress fluctuations measured along the flap chord when the flap deflection angle is progressively increased. Then, steady blowing is applied and its effect on wall shear stress fluctuations is analysed. For both controlled and uncontrolled cases, flow separation criteria are defined, studied and compared.

Reçu le :
Accepté le :
Publié le :
DOI : 10.1016/j.crme.2014.01.013
Keywords: Flow separation, Flow control, Flap, Steady blowing
Mot clés : Décollement, Contrôle des écoulements, Volet, Soufflage continu
Timothée Chabert 1 ; Julien Dandois 1 ; Éric Garnier 1 ; Laurent Jacquin 1

1 Onera – The French Aerospace Lab, 8, rue des Vertugadins, 92190 Meudon, France
@article{CRMECA_2014__342_6-7_389_0,
     author = {Timoth\'ee Chabert and Julien Dandois and \'Eric Garnier and Laurent Jacquin},
     title = {Experimental detection of flow separation over a plain flap by wall shear stress analysis with and without steady blowing},
     journal = {Comptes Rendus. M\'ecanique},
     pages = {389--402},
     publisher = {Elsevier},
     volume = {342},
     number = {6-7},
     year = {2014},
     doi = {10.1016/j.crme.2014.01.013},
     language = {en},
}
TY  - JOUR
AU  - Timothée Chabert
AU  - Julien Dandois
AU  - Éric Garnier
AU  - Laurent Jacquin
TI  - Experimental detection of flow separation over a plain flap by wall shear stress analysis with and without steady blowing
JO  - Comptes Rendus. Mécanique
PY  - 2014
SP  - 389
EP  - 402
VL  - 342
IS  - 6-7
PB  - Elsevier
DO  - 10.1016/j.crme.2014.01.013
LA  - en
ID  - CRMECA_2014__342_6-7_389_0
ER  - 
%0 Journal Article
%A Timothée Chabert
%A Julien Dandois
%A Éric Garnier
%A Laurent Jacquin
%T Experimental detection of flow separation over a plain flap by wall shear stress analysis with and without steady blowing
%J Comptes Rendus. Mécanique
%D 2014
%P 389-402
%V 342
%N 6-7
%I Elsevier
%R 10.1016/j.crme.2014.01.013
%G en
%F CRMECA_2014__342_6-7_389_0
Timothée Chabert; Julien Dandois; Éric Garnier; Laurent Jacquin. Experimental detection of flow separation over a plain flap by wall shear stress analysis with and without steady blowing. Comptes Rendus. Mécanique, Volume 342 (2014) no. 6-7, pp. 389-402. doi : 10.1016/j.crme.2014.01.013. https://comptes-rendus.academie-sciences.fr/mecanique/articles/10.1016/j.crme.2014.01.013/

[1] J.P. Stack, S.M. Mangalam, V. Kalburgi, The phase reversal phenomenon at flow separation and reattachment, AIAA Paper 88-0408.

[2] A. Nakayama, J.P. Stack, J.C. Lin, W.O. Valarezo, Surface hot-film method for the measurement of transition, separation, and reattachment points, AIAA Paper 1993-2918.

[3] N.O. Packard; J.P. Bons Closed-loop separation control of unsteady flow on an airfoil at low reynolds number, 2012 (AIAA Paper 2012-0754)

[4] J. Poggie; C.P. Tilmann; P.M. Flick; J.S. Silkey; B.A. Osbourne; Gregory Ervin; D. Maric; S. Mangalam; A. Mangalam Closed-loop stall control system, J. Aircraft, Volume 47 (2010) no. 5, pp. 1747-1755

[5] C. Rethmel, J. Little, K. Takashima, A. Sinha, I. Adamovich, M. Samimy, Flow separation control over an airfoil with pulse driven DBD plasma actuators, AIAA Paper 2011-487.

[6] T. Shaqarin; C. Braud; S. Coudert; M. Stanislas Open and closed-loop experiments to identify the separated flow dynamics of a thick turbulent boundary layer, Exp. Fluids, Volume 54 (2013), p. 1448

[7] V. Troshin; A. Seifert Performance recovery of a thick turbulent airfoil using a distributed closed-loop flow control system, Exp. Fluids, Volume 54 (2013), p. 1443

[8] L.G. Pack; N.W. Schaeffler; C.S. Yao; A. Seifert Active control of flow separation from supercritical airfoil leading-edge flap shoulder, J. Aircr., Volume 42 (2005) no. 5, pp. 1142-1149 (first presented as AIAA Paper 2002-3156)

[9] A. Seifert; L.G. Pack-Melton Control and identification of turbulent boundary layer separation, Proceedings of the IUTAM Symposium on One Hundred Years of Boundary Layer Research, 2006

[10] A. Meijering, W. Schroder, Experimental analysis of separated transitional transonic airfoil flow, AIAA Paper 2001-2987.

[11] C. Cuvier; C. Braud; J.-M. Foucaut; M. Stanislas Flow control over a ramp using active vortex generators, Proc. 7th Int. Symp. on Turbulence and Shear Flow Phenomena, 2011

[12] T. Chabert; J. Dandois; E. Garnier; L. Jacquin Experimental detection of a periodically forced turbulent boundary layer separation, Exp. Fluids, Volume 54 (2013), p. 1430

[13] F. Gand; S. Deck; V. Brunet; P. Sagaut Flow dynamics past a simplified wing body junction, Phys. Fluids, Volume 22 (2010) (115111)

[14] V. Brion Stabilité des paires de tourbillons contra-rotatifs : application au tourbillon de jeu dans les turbomachines, École polytechnique, Palaiseau, France, 2009 (PhD thesis)

[15] P. Poisson-Quinton; L. Lepage Survey of French research on the control of boundary layer and circulation (G.V. Lachmann, ed.), Boundary Layer and Flow Control, vol. 1, Pergamon Press, 1961

[16] R. Becker; R. King; R. Petz; W. Nitsche Adaptive closed-loop separation control on a high-lift configuration using extremum seeking, AIAA J., Volume 45 (2007) no. 6, pp. 1382-1392

[17] S.F. Hoerner; H. Borst Fluid-Dynamic Lift, Mrs Liselotte A. Hoerner, Brick Town, NJ, 1975

[18] G.A. Williamson Experimental wind tunnel study of airfoils with large flap deflections at low Reynolds numbers, University of Illinois at Urbana-Champaign, IL, USA, 2012 (Master thesis)

[19] R.L. Simpson; M. Ghodbane; B.E. McGrath Surface pressure fluctuations in a separating turbulent boundary layer, J. Fluid Mech., Volume 177 (1987), pp. 167-186

[20] K.B.M.Q. Zaman; D.J. McKinzie; C.L. Rumsey A natural low-frequency oscillation of the flow over an airfoil near stalling conditions, J. Fluid Mech., Volume 202 (1989), pp. 403-442

[21] J.H. Almutairi; I.M. AlQadi Large-eddy simulation of natural low-frequency oscillations of separating – reattaching flow near stall conditions, AIAA J., Volume 51 (2013) no. 4, pp. 981-991

[22] J.-Z. Wu; X.-Y. Lu; A.G. Denny; M. Fan; J.-M. Wu Post-stall flow control on an airfoil by local unsteady forcing, J. Fluid Mech., Volume 371 (1998), pp. 21-58

[23] T. Chabert Contrôle expérimental en boucle fermée du décollement sur un volet, Université Pierre et Marie Curie, Paris VI, France, 2014 (PhD thesis)

Cité par Sources :

Commentaires - Politique


Ces articles pourraient vous intéresser

Stall control with feathers: Self-activated flaps on finite wings at low Reynolds numbers

C.H. John Wang; Jörg Schlüter

C. R. Méca (2012)


Stroke plane angle controls leading edge vortex in a bat-inspired flapper

Gide Koekkoek; Florian T. Muijres; L. Christoffer Johansson; ...

C. R. Méca (2012)


Control of vortex shedding on a circular cylinder using self-adaptive hairy-flaps

Sebastian Kunze; Christoph Brücker

C. R. Méca (2012)