SACCON CFD static and dynamic derivatives using elsA

28th AIAA Applied Aerodynamics Conference

Volumn 1, Issue , 2010, Pages

  Le Roy, J F ^a,b   Morgand, S ^a,b  

^a ONERA   (France)

^b Department of Applied Aerodynamics ^*  (France)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; SWEPT WINGS; WIND TUNNELS;

BLENDED WING BODY; CFD APPROACHES; COMPLEX DYNAMIC BEHAVIOR; DYNAMIC DERIVATIVES; NON-LINEAR AERODYNAMICS; OFF DESIGN CONDITION; PRESSURE COEFFICIENTS; STABILITY AND CONTROL;

COMPUTATIONAL FLUID DYNAMICS;

EID: 78649499187     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2010-4562     Document Type: Conference Paper

References (14)

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2. Gursul, I., Gordnier, R., and Visbal., M., "Unsteady Aerodynamics of Nonslender Delta Wings", Progress in Aerospace Sciences, 2005, 41 pp 515-557. (Pubitemid 41817298)
3. Riou, J., "Etudes et contrôle du décrochage d'ailes et gouvernes de missile en régime transsonique", Thesis, University of Paris XIII, France, 2009.
4. th Fluid Dynamics Conference and Exhibit, Chicago, IL, 2010.
5. th Fluid Dynamics Conference and Exhibit, Chicago, IL, 2010.
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7. th AIAA Aerospace Science Meeting and Exhibit, Reno (USA), January 7-11, 2008.
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9. Head of interface, "elsA Theoretical Manuel", 2008
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13. th Applied Aerodynamics Conference, AIAA 2006-2989, San Francisco, California, June 5-8, 2006.
14. Mitchell, A., M. "Caractérisation et Contrôle de l'Eclatement Tourbillonnaire sur Aile Delta aux Hautes Incidences", Thesis, University of Paris VI, France, Département de Mécanique, juillet 2000.