Hostname: page-component-77c89778f8-gq7q9 Total loading time: 0 Render date: 2024-07-18T16:26:26.406Z Has data issue: false hasContentIssue false
  • English
  • Français

An overview of flow control activities at Dassault Aviation over the last 25 years

Part of: RAeS Lanchester Lecture Papers

Published online by Cambridge University Press:  23 March 2016

J.-P. Rosenblum
J.-P. Rosenblum*
Affiliation:
Dassault Aviation, Direction Générale Technique, Saint-Cloud, France
*
jean-pierre.rosenblum@dassault-aviation.com
Get access Rights & Permissions [Opens in a new window]

Abstract

In France, the very first ideas on flow control were developed by Philippe Poisson-Quinton from the Office National d'Etudes et Recherches Aérospatiales (ONERA) in the 1950s. There was some renewal of this research topic in the early 1990s, first in the United States with scientists like Wygnanski and Gad-El Hak, and also in France at the initiative of Pierre Perrier from Dassault Aviation, who triggered a lot of research activities in this field both at ONERA and in the French National Centre for Scientific Research (CNRS) laboratories. The motivation was driven by the applications on Dassault Aviation military aircraft and Falcon business jets in order to contribute to the design, while facilitating performance optimisation and multi-disciplinary compromise. A few examples of flow control technologies, such as forebody vortex control, circulation control, flow separation control or boundary layer transition control using hybrid laminar flow control (HLFC), are presented to illustrate the applications and to explain the methodology used for the design of the flow control devices. The author also emphasises the current reaction of industry with respect to the integration of flow control technologies on an aircraft programme. The conclusion is related to the present status of the French research on this topic and to the next challenges to be addressed.

Keywords

Flow controlfluid dynamics
Type
Research Article
Information
The Aeronautical Journal , Volume 120 , Issue 1225 , March 2016 , pp. 391 - 414
Copyright
Copyright © Royal Aeronautical Society 2016 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1.Rebuffet, P. and Poisson-Quinton, P. Recherches sur l'hypersustentation d'une aile en flèche réelle par contrôle de la couche limite utilisant le prélèvement d'air sur le turbo-réacteur, La Recherche aéronautique, March-April 1950, 14.Google Scholar
2.Malavard, L., Poisson-Quinton, P. and Jousserandot, P. Recherches théoriques et expérimentales sur le contrôle de circulation par soufflage appliqué aux ailes d'avions. 1956, ONERA Report.Google Scholar
3.Poisson-Quinton, P. Recherches théoriques et expérimentales sur le contrôle de couche limite, 7th Congress of Applied Mechanics, September 1948, London, UK.Google Scholar
4.Werle, H.Visualisation hydrodynamique de l’écoulement autour d'un cylindre profilé avec aspiration, maquette de la turbovoile Cousteau – Malavard. La Recherche aérospatiale, 1984, (4), pp 265–274.Google Scholar
5.Seifert, A., Bachar, T., Koss, D., Wygnanski, I. and Shepshelovich, M.Oscillatory blowing – a tool to delay boundary layer separation, AIAA J., 1993, 31, pp 2052–2060.Google Scholar
6.Glezer, A. and Amitay, M.Synthetic jets. Annual Review of Fluid Mechanics, 2002, 34, (1), pp 503–529.Google Scholar
7.Perrier, P.Multiscale Active Flow Control, Flow Control: Fundamentals and Practices, Carghese, Corsica conference, 1998, GAD-EL-HAK, M., POLLARD, A. and BONNET (Eds), J.-P., Springer-Verlag, pp 275–334.Google Scholar
8.Courty, J.-C. and Van, T.D. Military aircraft control at high angle-of-attack, CEAS European Forum on High Lift and separation control, March 1995, University of Bath, Bath, UK.Google Scholar
9.Rosenblum, J.-P., Courty, J.-C. and Van, T.D. Contrôle des avions militaires aux incidences élevées, 1996, AAAF, Ecole centrale de Lyon, Lyon, France.Google Scholar
10.Courty, J.-C. Industrial Constraints and Requirements for Aeronautical Flow Control Applications, March 2009, Von Karman Institute for Fluid Dynamics, Lecture Series 2009-02.Google Scholar
11.Lanchester, F.W. Aerial Flight, 1907 Constable & Co. Ltd., London, UK.Google Scholar
12.Whitmore, I., Weatherhill, K., Stevens, K.,Green, J., Vallee, J.J., Bourasseau, M. and Massonnat, J.M. The application of flow control to ahighly convoluted air intake duct for a combat UAV, Royal Aeronautical Society Applied Aerodynamics, July 2012, Conference in Bristol, Bristol, UK.Google Scholar
13.Dandois, J., Molton, P., Lepage, A., Geeraert, A., Brunet, V., Dor, J.-B. and Coustols, E.Buffet characterization and control for turbulent wings, AerospaceLab J., 2013, AL06-1, 1–17.Google Scholar
14.Bulgubure, C. and Arnal, D. Dassault Aviation Falcon 50 Laminar Flow Flight Demonstrator, First European Forum on Laminar Flow Technology, 16-18 March 1992, Hamburg, Germany.Google Scholar
15.Courty, J.-C., Bulgubure, C. and Arnal, D. Laminar flow investigation: computations and flight tests at Dassault Aviation, Recent Advances in Long Range and Long Endurance Operation of Aircraft, AGARD Conference Proceedings 547, 24-27 May 1993, TheHague, Netherlands.Google Scholar
16.Arnal, D. Recent advances in theoretical methods for laminar-turbulent transition prediction, 36th Aerospace Sciences Meeting & Exhibit, AIAA 98-0223, 12-15 January 1998, Reno, Nevada, US.Google Scholar
17.Casalis, G. Laminar-Turbulent transition induced by instability mechanisms: overview of the current methods studied at ONERA, ECCOMAS 98 Conference, 7-11 September 1998, Athens, Greece.Google Scholar
18.Arnal, D. and Archambaud, J.-P. Laminar-Turbulent transition control: NLF, LFC, HLFC, RTO-AVT/VKI Lecture Series, Advances in laminar-turbulent transition modelling, 2008.Google Scholar
19.Arnal, D., Casalis, G. and Houdeville, R. Practical transition prediction methods: subsonic and transonic flows, RTO-AVT/VKI Lecture Series, Advances in laminar-turbulent transition modelling, 2008.Google Scholar
20.Courty, J.-C., Tran, D. and Petit, G. In Flight Infra Red measurements of localized details impact on laminarity, 3AF, 48th International Symposium of Applied Aerodynamics, March 2013, Saint-Louis, France.Google Scholar
21.Gross, R., Courty, J.-C., Tran, D., Mallet, M., Arnal, D. and Vermeersch, O. Prediction of laminar/turbulent transition in an unstructured finite element Navier Stokes solver using a boundary layer code, 3AF, 50th International Conference of Applied Aerodynamics, March/April 2015, Toulouse, France.Google Scholar