Comparison of measured and simulated flow features for the full-scale F-16XL aircraft

Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting

Volumn 9, Issue , 2007, Pages 5879-5895

  Boelens, O J ^a,b   Spekreijse, S P ^a,c   Sytsma, H A ^a,b   De Cock, K M J ^a,d  

^a NATIONAL AEROSPACE LABORATORY NLR   (Netherlands)

^b Applied Computational Ruid Dynamics   (Netherlands)

^c Applied Computational Ruid Dynamics

^d Aerospace Vehicles Division   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

FLIGHT TEST DATA; FLOW SIMULATION SYSTEM; FLOW SOLVERS; GRID GENERATION TOOLS;

ALGORITHMS; COMPUTATIONAL FLUID DYNAMICS; FLIGHT DYNAMICS; NASA; PROJECT MANAGEMENT; WIND TUNNELS;

FIGHTER AIRCRAFT;

EID: 34250890148     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (22)

1. Lamar, J.E., Obara, C.J., Fisher, B.D, and Fisher, D.F., "Flight, wind-tunnel, and Computational Fluid Dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds", NASA TP-2001-210629, 2001.
2. Hummel, D., and Redeker, G., "A new vortex flow experiment for computer code validation. Presented at RTO AVT Symposium on Advanced Flow Management; Part A - Vortex Flow and High Angle of Attack, Paper Number 8, in Loen Norway during May 7-11, 2001.
3. th AIAA Aerospace Sciences Meeting and Exhibit, Reno NV, January 8-11, 2007.
4. th AIAA Aerospace Sciences Meeting and Exhibit, Reno NV, January 8-11, 2007.
5. th AIAA Aerospace Sciences Meeting and Exhibit, Reno NV, January 8-11, 2007.
6. th AIAA Aerospace Sciences Meeting and Exhibit, Reno NV, January 8-11, 2007.
7. th AIAA Aerospace Sciences Meeting and Exhibit, Reno NV, January 8-11, 2007.
8. th AIAA Aerospace Sciences Meeting and Exhibit, Reno NV, January 8-11, 2007.
9. th AIAA Aerospace Sciences Meeting and Exhibit, Reno NV, January 8-11, 2007.
10. th AIAA Aerospace Sciences Meeting and Exhibit, Reno NV, January 8-11, 2007.
11. th AIAA Aerospace Sciences Meeting and Exhibit, Reno NV, January 8-11, 2007.
12. th AIAA Aerospace Sciences Meeting and Exhibit, Reno NV, January 8-11, 2007.
13. Lamar, J.E. and Abdol-Hamid, K.S., "USM3D unstructured grid solutions for CAW API at NASA LaRC", AIAA-2007-0682, Presented at 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno NV, January 8-11, 2007.
14. th AIAA Aerospace Sciences Meeting and Exhibit, Reno NV, January 8-11, 2007.
15. "ENFLOW: A computer code system for accurate simulation of three-dimensional flows", URL: http://www.nlr.nl/documents/flyers/f222- 01.pdf [cited 12 December 2006].
16. Spekreijse, S.P., Prananta, B.B. and Kok, J. C., "A simple, robust and fast algorithm to compute deformations of multi-block structured grids", NLR-TP-2002-105, 2002.
17. Kok, J.C., "Resolving the dependence on free-stream values for the k-ω turbulence model", NLR-TP-99295. 1999.
18. Brandsma, F.J., Kok, J.C, Dol, H.S. and Elsenaar, A., "Leading edge vortex flow computations and comparison with DNW-HST wind tunnel data", NLR-TP-2001-238, 2001.
19. Dol, H.S., Kok, J.C. and Oskam, B., "Turbulence modeling for leading-edge vortex flows", AIAA-2002-0843, 2002.
20. Kok, J.C., Dol, H.S., Oskam, B., and van der Ven, H., "Exra-large eddy simulation of massively separated flows", NLR-TP-2003-200, 2003.
21. th International Congress of the Aeronautical Sciences, Yokohama, Japan, August 29 - September 3, 2004.
22. Boelens, O.J. "Feature-based code validation using F-16XL flight test and wind tunnel data", Submitted to AVT-147 Symposium on Computational Uncertainty, Athens, Greece, 1-4 October 2007.