Comparison of measured and block structured simulation results for the F-16XL aircraft

Journal of Aircraft

Volumn 46, Issue 2, 2009, Pages 377-384

  Boelens, O J ^a,f   Badcock, K J ^b,g   Elmilgui, A ^c   Abdol Hamid, K S ^d,h   Massey, S J ^e  

^a NATIONAL AEROSPACE LABORATORY NLR   (Netherlands)

^b UNIVERSITY OF LIVERPOOL   (United Kingdom)

^c ANALYTICAL SERVICES AND MATERIALS INC   (United States)

^d NASA LANGLEY RESEARCH CENTER   (United States)

^e Eagle Aeronautics   (United States)

^f Aerospace Vehicles Division   (Netherlands)

^g Department of Engineering ^*  (United Kingdom)

^h Distinguished Research Associate   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; CODES (SYMBOLS); COMPUTATIONAL FLUID DYNAMICS; NAVIER STOKES EQUATIONS; RESEARCH AIRCRAFT; TWO PHASE FLOW; VORTEX FLOW;

ALGEBRAIC STRESS MODEL; COMPUTATIONAL FLUID DYNAMICS CODES; FIGHTER CONFIGURATION; FLIGHT CONDITIONS; REYNOLDS AVERAGED NAVIER STOKES CODES; STRUCTURED MULTIBLOCK GRIDS; SURFACE PRESSURES; UNSTEADY REYNOLDS-AVERAGED NAVIER-STOKES;

SUPERSONIC AIRCRAFT;

EID: 63349102583     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.35064     Document Type: Article

References (16)

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. Obara, C. J., and Lamar, J. E., "Overview of the Cranked-Arrow Wing Aerodynamics Project International," Journal of Aircraft, Vol. 46, No. 2, 2009, pp. 355-368. doi:10.2514/34957
3. Boelens, O. J., Badcock, K. J., Görtz, S., Morton, S., Fritz, W., Karman, S. L., Jr., Michal, T., and Lamar, J. E., "Description of the F-16XL Geometry and Computational Grids Used in CAWAPI," Journal of Aircraft, Vol. 46, No. 2,2009, pp. 369-376. doi:10.2514/34852
4. Goertz, S., Jirasek, A., Morton, S. A., McDaniels, D. R., Cummings, R. M., Lamar, J. E., and Abdol-Hamid, K. S., "Standard Unstructured Grid Solutions for CAWAPI F-16XL," Journal of Aircraft, Vol. 46, No. 2, 2009, pp. 385-408. doi:10.2514/35163
5. Fritz, W., Davis, M. B., Karman, S. L., Jr., and Michal, T., "RANS Solutions for the CAWAPI F-16XL Using Different Hybrid Grids," Journal of Aircraft, Vol. 46, No. 2, 2009, pp. 409-422. doi:10.2514/35106
6. Rizzi, A., Jirasek, A., Badcock, K. J., Lamar, J. E., Boelens, O. J., and Crippa, S., "What Was Learned from Numerical Simulations of F-16XL (CAWAPI) at Flight Conditions," Journal of Aircraft, Vol. 46, No. 2, 2009, pp. 423-441. doi:10.2514/35698
7. Hummel, D., and Redeker, G., "A New Vortex Flow Experiment for Computer Code Validation," RTO-A VTSymposium on Advanced Flow Management; Part A-Vortex Flow and High Angle of Attack Papers on Disc [CD-ROM], Paper 8, NATO, Neuilly sur Seine, France, May 2001.
8. Boerstoel, J. W., Kassies, A., Kok, J. C., and Spekreijse. S. P., "ENFLCW, a Full-Functionality System of CFD Codes for Industrial Euler/Navier-Stokes Flow Computations," National Aerospace Laboratory TP-96286U, Amsterdam, 1996.
9. Badcock, K. J., Richards, B. E., and Woodgate, M. A., "Elements of Computational Fluid Dynamics on Block Structured Grids using Implicit Solvers," Progress in Aerospace Sciences, Vol. 36, No. 5-6, Aug. 2000, pp. 351-392. doi:10.1016/S0376-0421(00)00005-1
10. Abdol-Hamid, K., Pao, S. P., Hunter, C., Deere, K. A., Massey, S. J., and Elmiligui, A., "PAB3D: Its History in the Use of Turbulence Models in the Simulation of Jet and Nozzle Flows," AIAA Paper 2006-489, 2006.
11. Nichols, R. H., and Nelson, C. C., "Application, of Hybrid RANS/LES Turbulence Models," AIAA Paper 2003-83, 2003.
12. Abdol-Hamid, K., and Girimaji, S., "A Two-Stage Procedure Toward the Efficient Implementation of PANS and Other Hybrid Turbulence Models," NASA TM-213260, 2004.
13. Kok, J. C., "Resolving the Dependence on Free-Stream Values for the k-ω Turbulence Model," National Aerospace Laboratory TP-99295, Amsterdam, 1999.
14. Shih, T. H., Zhu, J., and Lumley, J. L., "A New Reynolds Stress Algebraic Equation Model," NASA TM-106644, Aug. 2004.
15. Brandsma, F. J., Kok, J. C.,Dol, H. S., andElsenaar, A., "Leading Edge Vortex Flow Computations and Comparison with DNW-HST Wind Tunnel Data," National Aerospace Laboratory TP-2001-238, Amsterdam, 2001.
16. Dol, H. S., Kok, J. C., and Oskam, B., "Turbulence Modeling for Leading-Edge Vortex Flows," AIAA Paper 2002-0843, 2002.