Towards the simulation of unsteady manoeuvre dominated by vortical flow

21st AIAA Applied Aerodynamics Conference

Volumn , Issue , 2003, Pages

  Soemarwoto, B I ^a   Boelens, O J ^a   Allan, M ^b   Arthur, M T ^c   Butefisch K ^d   Ceresola, N ^e   Fritz, W ^f  

^a NATIONAL AEROSPACE LABORATORY NLR   (Netherlands)

^b UNIVERSITY OF GLASGOW   (United Kingdom)

^c QINETIQ   (United Kingdom)

^d GERMAN AEROSPACE CENTER DLR   (Germany)

^e ALENIA SPAZIO   (Italy)

^f AIRBUS GROUP INNOVATIONS   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

DELTA WING AIRCRAFT; NAVIER STOKES EQUATIONS; TRANSONIC AERODYNAMICS; TURBULENCE MODELS; VORTEX FLOW;

COMPUTATIONAL RESULTS; LEADING-EDGE VORTICES; PRESSURE COEFFICIENTS; ROTATIONAL RATES; TOTAL-PRESSURE LOSS; TURBULENCE INTENSITY; UNIVERSITY OF GLASGOW; UNSTEADY REYNOLDS-AVERAGED NAVIER-STOKES;

COMPUTATIONAL FLUID DYNAMICS;

EID: 85067317302     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-3528     Document Type: Conference Paper

References (24)

1. B.R. Williams, W. Kordulla, M. Borsi, and H.W.M. Hoeij-makers. Comparison of solution of various Euler solvers and one Navier-Stokes solver for the flow about a sharp-edged cropped delta wing. AGARD-CP-494, 1994.
2. Hilgenstock, W. Kordulla, and A. Meister. Common Exercise II on the IEPG delta wing WI1-SLE Navier-Stokes and Euler+ solutions on the common Aermacchi C-H-Grid. DLR-IB 221-93 C 12, 1993.
3. M.T. Arthur. WEAG TA-15 Common Exercise III on grid adaptation in vortical flow simulations, Part I: Euler solutions. DRA/AS/ASD/TR96073/1, April 1997.
4. M.T. Arthur. WEAG TA-15 Common Exercise III on grid adaptation in vortical flow simulations, Part II: Navier-Stokes solutions. DRA/AS/ASD/SP97550/1.0, December 1997.
5. M.T. Arthur, W. Kordulla, F.J. Brandsma, and N. Ceresola. Grid adaptation in vortical flow simulations. AIAA Paper 97-2308, 1997.
6. N. Ceresola. WEAG-TA15 Common Exercise IV -Time accurate Euler calculations of vortical flow on a delta wing in pitch motion. Alenia Report 65/RT/TR302/98182, 1998.
7. M.T. Arthur, F.J. Brandsma, N. Ceresola, and W. Kordulla. Time accurate euler calculations of vortical flow on a delta wing in pitching motion. AIAA Paper 99-3110, 1999.
8. W. Fritz. WEAG TA 15 Common Exercise V. DASA Report Dasa/S/STY/1820, 2000.
9. W. Fritz, M.T. Arthur, F.J. Brandsma, K.-A. Bütefisch, and N. Ceresola. Time accurate euler calculations of vortical flow over a delta wing in rolling motion. RTO/AVT Vortex Flow Symposium, Loen, Norway, 2001.
10. N. Kroll, P. Aumann, W. Bartelheimer, H. Bleecke, B. Eis-feld, J. Lieser, R. Heinrich, M. Kuntz, E. Monsen, J. Raddatz, U. Reisch, and B. Roll. FLOWer Installation and User Handbook. DLR Doc.Nr.:MEGAFLOW-1001, 1998.
11. D. C. Wilcox. Turbulence Modelling for CFD. DCW Industries, 1998.
12. J.C. Kok. Resolving the dependence on freestream values for the k-ω turbulence model. AIAA Journal, 38(7):1292-1294, 2000.
13. J.C. Kok and S.P. Spekreijse. Efficient and accurate implementation of the k-ω turbulence model in the NLR multi-block Navier-Stokes system. NLR TP-2000-144 (presented at ECCO-MAS 2000, Barcelona, Spain, 11-14 September, 2000), 2000.
14. F.J. Brandsma, J.C. Kok, Dol H.S., and A. Elsenaar. Leading edge vortex flow computations and comparison with DNW-HST wind tunnel data. RTO/AVT Vortex Flow Symposium, Loen, Norway
15. J.W. Boerstoel, A. Kassies, J.C. Kok, and S.P. Spekreijse. ENFLOW, A full-functionality system of CFD codes for industrial Euler/Navier-Stokes Flow Computations. NLR TP 96286, 1996.
16. S. Osher and S.R. Chakravarthy. Upwind schemes and boundary conditions with applications to euler equations in general coordinates. J. Computational Physics, 50:447-481, 1983.
17. F. Cantariti, L. Dubuc, B. Gribben, M. Woodgate, K.J. Badcock, and B.E. Richards. Approximate Jacobians for the solution of the Euler and Navier-Stokes equations. Glasgow University Aero report 5, 1997.
18. F. Cantariti, M. Woodgate, K. Badcock, and B. Richards. Solution of the Navier-Stokes Equations in Three dimensions using a fully unfactored method. Glasgow University Aero report 9908, 1999.
19. Jameson. Time dependent calculations using multigrid with application to unsteady flows past airfoils and wing. AIAA Paper 91-1596, 1991.
20. K.J. Badcock, F. Cantariti, L. Dubuc, and B.E. Richards. Simulation of unsteady turbulent flows around moving aerofoils using the pseudo time method. Int. J. Num. Meth. Fluids, 32:584-604, 2000.
21. V. Selmin. The node-centred finite volume approach: bridge between finite difference and finite elements. Comp. Meth. Appl. Mech. Eng., 102:107-138, 1993.
22. R.H. Engler and Ch. Klein. First results using the new DLR PSP system - intensity of lifetime measurements. Wind Tunnels and Wind Tunnel Test Techniques, 14-16 April 1997, Cambridge, UK, 1997.
23. R.H. Engler, Ch. Klein, E. Merlo, and P. van Amerom. 360° PSP measurements in transonic flow. 19th ICIASF Congress, Cleveland, Ohio, USA, pages 149-158, 2001.
24. R. Engler, S. Fonov, C. Klein, K-A. Bütefisch, D. Weiskat, K-W. Bock, and W. Fritz. Study of unsteady behaviour of a rotating 65° delta wing at M = 0.8 using pressure sensitive paint (PSP). RTO/AVT Vortex Flow Symposium, Loen, Norway, 2001.