Review of ONERA aerodynamic research in support of a future supersonic transport aircraft

Progress in Aerospace Sciences

Volumn 36, Issue 8, 2000, Pages 581-627

  Thibert, J J ^a   Arnal, D ^b  

^a ONERA   (France)

^b Aerodyn Energetics Models Dept   (France)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; DRAG; FLOW CONTROL; FRICTION; INTAKE SYSTEMS; LAMINAR FLOW; SUPERSONIC AERODYNAMICS; WIND TUNNELS; WINGS;

SUPERSONIC TRANSPORT AIRCRAFTS;

SUPERSONIC AIRCRAFT;

EID: 0034324233     PISSN: 03760421     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0376-0421(00)00010-5     Document Type: Review

References (43)

1. Seebass R, Woodhull JR. History and economics of and prospects for commercial supersonic transport. RTO-EN-4, Paper No. 1, November 1998.
2. Mizuno H. Japanese study on market prospect for future SST/HST. Paper II, 2.2.C, Strasbourg, November 1989.
3. Whitehead Jr AH. Status of NASA high-Speed research programme. RTO-EN-4, Paper No 10, November 1998.
4. Yoshida K. Overview of NAL'S program including the aerodynamic design of the scaled supersonic experimental airplane. RTO-EN-4, Paper No. 15, November 1998.
5. Vuillot AM, Couailler V, Liamis N. 3D turbomachinery Euler and Navier-Stokes calculations with a multidomain cell-centred approach. AIAA Paper 93-2576, Monterey, 1993.
6. Lerat A, Sides J, Daru V. An implicit finite volume method for solving the Euler equations. Lecture Notes in Physics, vol. 17. Berlin: Springer, 1982. p. 343-9.
7. Jameson A, Schmidt W, Turkel E. Numerical solution of the Euler equations by finite volume methods. AIAA Paper 81-1259, 1981.
8. Houdeville R. Three-dimensional boundary layer calculation by a characteristic method using Runge-Kutta time stepping schemes. Proceedings of the Fifth Symposium on Numerical and Physical Aspects of Aerodynamic Flows, Long Beach, January 1992.
9. Lovell DA. European Research to reduce drag for supersonic transport aircraft. AIAA Paper 99-3100.
10. Elsenaar A. Wind tunnel test of the EUROSUP SCT configuration. EUROSUP/NLR/T017/1.
11. Coustols E, Arnal D, Computations of laminar-transitional-turbulent flows over supersonic aircraft: skin friction prediction and reduction. NAL International Workshop for Supersonic Transport Design, Tokyo, March 1998.
12. Coustols E, Cottet Ph. Analysis of local friction measurements performed on a Concorde aircraft: inviscid and viscous computations. Proceedings, 7e Conférence Européenne Aérospatiale sur le Transport Supersonique de Seconde Génération, Toulouse, Labège, October 1994.
13. Thibert JJ. One point and multi-point design optimisation for airplane and helicopter application. AGARD FDP/VKI Special course on Inverse Methods for Airfoil Design for Aeronautical and Turbomachinery. Applications. AGARD Report No. 780, Paper No. 10.
14. Destarac D, Reneaux J. Applications de l'optimisation numérique à l'aérodynamique des avions de Transport. La Recherche Aerospatiale 1993;(2):39-55.
15. Vanderplaats Garret N. CONMIN - a fortran program for constrained function minimization. NASATMX 62, 282 - August 1973.
16. Vanderplaats Garret N. COPES - a fortran control program for engineering synthesis.
17. Grenon R. Numerical optimization in aerodynamic design with application to a supersonic transport aircraft. NAL International Workshop on Supersonic Transport Design, Tokyo, March 1998.
18. Reneaux J, Thibert JJ, Schmitt V. ONERA activities on drag reduction. ICAS Paper 90-3.6.1.
19. Schmitt V, Hinsinger R. Advanced transport aircraft aerodynamics in cooperation with Airbus Industrie. La Recherche Aerospatiale 1996;(4):265-77.
20. Coustols E, Schmitt V. In: Synthesis of experimental Riblet studies in transonic conditions in turbulence control by passive means. Coustols E, editor. Dordrecht: Kluwer Academic Publisher, 1990.
21. Robert JP. Drag reduction: an industrial challenge. AGARD Report 786, Special Course on Skin Friction Drag Reduction, March 1992.
22. Coustols E, Cousteix J. Performances of riblets in the Supersonic regime. AIAA 32(2). Technical notes. 1994;431-3.
23. Mack LM. Boundary layer linear stability theory. AGARD Report No. 709, 1984.
24. Smith AMO, Gamberoni N. Transition, pressure gradient and stability theory. Report ES 26388, Douglas Aircraft Co., El Segundo, CA, 1956.
25. Van Ingen JL. A suggested semi-empirical method for the calculation of boundary layer transition region. Report UTH-74, University of Technology Department of Aero. Engineering, Delft, 1956.
26. Arnal D. Boundary layer transition predictions based on linear theory. AGARD FDP/VKI Special Course on Progress in Transition Modelling - AGARD Report No. 793.
27. Fisher DF, Dougherty NS. In-flight transition measurements on a 10 deg. cone at Mach numbers from 0.5 to 2. TP 1971, NASA, 1982.
28. Coustols E. Stabilité et transition en écoulement tridimensionnel: cas des ailes en flèche. Thèse de Docteur-Ingénieur ENSAE (Juin 1983).
29. Arnal D. Transition prediction in transonic flow. IUTAM Symposium Transsonicum III. DFVLR - AVA Göttingen, 1988.
30. Lemee P. Laminar flow applications for supersonic aircraft. Dragnet, European Drag Reduction Wokshop, Toulouse, June 1999.
31. Beckwith I.E. Development of high Reynolds number quiet tunnel for transition research. AIAA J. 13(3):1975;300-306.
32. Beckwith IE, Creel Jr TR, Chen FJ, Kendall JM. Freestream noise and transition measurements on a cone in a Mach 3.5 pilot low-disturbance tunnel. TP 2180, NASA, 1983.
33. Papirnik O, Rancarani G, Delery J, Arnal D. Conception et qualification de la soufflerie silencieuse R1Ch de l'ONERA. AGARD Conference on Aerodynamics of Wind Tunnel Circuits and their Components. MOSCOU 30/9-3/10, 1996-ONERA TP 1996-175.
34. Pfenninger W. Flow phenomena at the leading edge of swept wings. AGARDograph 97, Part 4, 1965.
35. Poll DIA. Some aspects of the flow near a swept attachment line with particular reference to boundary layer transition. Technical Report 7805/K, Cranfield, College of Aeronautics, August 1978.
36. Poll DIA. Boundary layer transition on the windward face of space shuttle during reentry. AIAA Paper 85-0899, 1985.
37. Reed HL, Kimmel R, Schneider S, Arnal D. Drag prediction and transition in hypersonic flow. AIAA Paper 97-1818, 1997.
38. Reneaux J, Preist J, Juillen JC, Arnal D. Control of attachment line contamination. Proceedings of the second European Forum on Laminar Flow Technology Bordeaux, France, June 10, 1996, ONERA TP 1996-84.
39. Arnal D, Vignau F, Laburthe F. Recent supersonic transition studies with emphasis on the swept cylinder case. Conference on Boundary layer Transition and Control, Cambridge, April 1991.
40. Leynaert J. Transport Aircraft intake design. VKI - Lecture Series 1988-04 Intake Aerodynamics - ONERA TP 1988-18.
41. e Colloque d'Aérodynamique Appliquée, Talence, October 1988, ONERA TP 1988-132.
42. Cambier L, Daracq D, Gazaix M, Guillen Ph, Jouet Ch, Le Toullec L. Améliorations récentes du code de calcul d'écoulement compressible FLU3M. AGARD Séville, Espagne, 2-5 October 1995.
43. Thierry G. Simulations d'écoulements de fluides parfaits autour de corps déformables. Applications à l'aéroélasticité des lanceurs. Thèse de doctorat de l'Université de Paris Nord, 1998.