Description of the F-16XL geometry and computational grids used in CAWAPI

Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting

Volumn 9, Issue , 2007, Pages 5866-5878

  Boelens, O J ^a,f   Goertz, S ^b   Morton, S ^c,g   Fritz, W ^d   Lamar, J E ^e,g,h  

^a NATIONAL AEROSPACE LABORATORY NLR   (Netherlands)

^b ROYAL INSTITUTE OF TECHNOLOGY   (Sweden)

^c UNITED STATES AIR FORCE ACADEMY   (United States)

^d AIRBUS GROUP INNOVATIONS   (Germany)

^e NASA LANGLEY RESEARCH CENTER   (United States)

^f Applied Computational Fluid Dynamics   (Netherlands)

^g AIAA   (United States)

^h EADS MAS ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL GRIDS; FLIGHT DATABASES; GEOMETRY DESCRIPTION; GRID GENERATION;

AEROSPACE ENGINEERING; AIRCRAFT MANUFACTURE; COMPUTATIONAL FLUID DYNAMICS; FLIGHT DYNAMICS;

WINGS;

EID: 34250893858     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (26)

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 CAWAPI 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. Samareh, S., "GridTool: A Surface Modeling and Grid Generation Tool", In Proceedings of the Workshop on Surface Modeling, Grid Generation, and Related Issues in CFD Solutions, NASA CP-3291, May 9-11, 1995.
18. Pirzadeh, S. "Progress toward a User-Oriented Unstructured Viscous Grid Generator", AIAA-96-0031, 1996.
19. Strang, W. Z., Tomaro, R. F., and Grismer, M. J., "The Defining Methods of Cobalt: A Parallel, Implicit, Unstructured Euler/Navier-Stokes Flow Solver", AIAA- 99-0786, 1999.
20. Wallin, S., "Standardized Data Format, The Aeronautical Research Institute of Sweden (FFA)", FFAP-A-950, Stockholm, Sweden, 1992.
21. Eliasson, P., "EDGE, a Navier-Stokes solver for unstructured grids", Proc. To Finite Volumes for Complex Applications III, ISBN 1 9039 9634 1, pp. 527-534, 2002.
22. Legensky, S. M., Edwards D. E., Bush R. H., Poirier D. M. A., Rumsey, C. L., Cosner R. R., and Towne, C. E., "CFD General Notation System (CGNS): Status and Future Directions", AIAA-2002-0752, 2002.
23. Lamar, J. E., Cronin, C. K, and Scott, L. E., "A review of steps taken to create an international virtual laboratory at NASA Langley for aerodynamic prediction and comparison", Progress in Aerospace Sciences, vol. 40, no. 3, pp. 163-172, April, 2004.
24. Gerhold, T., Friedrich, O., Evans, J., Galle, M., "Calculation of Complex Three-Dimensional Configurations Employing the DLR-Tau Code.", AIAA-97-0167, 1997
25. CentaurSoft Grid Generator, http://www.centaursoft.com [cited 19 December 2006].
26. Karman, S. Jr., "Unstructured Viscous Layer Insertion Using Linear-Elastic Smoothing," AIAA-2006-0531 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 9-12, 2006.