Numerical investigation of Reynolds number effects on a blunt leading-edge delta wing

Collection of Technical Papers - AIAA Applied Aerodynamics Conference

Volumn 2, Issue , 2006, Pages 708-726

  Crippa, Simone ^a,b,c   Rizzi, Arthur ^a,b,c  

^a ROYAL INSTITUTE OF TECHNOLOGY   (Sweden)

^b Dept of Aeronautical and Vehicle Engineering ^*  (Sweden)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE MEASUREMENT; COMPUTATIONAL FLUID DYNAMICS; DELTA WING AIRCRAFT; NUMERICAL METHODS; VORTEX FLOW; WIND TUNNELS;

MACH NUMBERS; SECONDARY SEPARATION; VORTEX STRENGTH;

REYNOLDS NUMBER;

EID: 33845409766     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-3001     Document Type: Conference Paper

References (16)

1. th AIAA Aerospace Sciences Meeting and Exhibit, 2002.
2. st AFSOR International Conference on DNS/LES, Advances in DNS/LES, Greyden Press, 1998.
3. Elsenaar, A. and Eriksson, G., editors, International Vortex Flow Experiment on Euler Code Validation. FFA, Flygtekniska Försö kanstalten, October 1986.
4. nd International Symposium on Integrating CFD and Experiments in Aerodynamics, Cranfield University (Shrivenham), UK, 2005, pp. 1-12.
5. th AIAA Aerospace Sciences Meeting and Exhibit, 2006.
6. Chu, J. and Luckring, J. M., "Experimental Surface Pressure Data Obtained on 65° Delta Wing Across Reynolds Number and Mach Number Ranges," Tech. rep., NASA Langley Research Center, Hampton, Virginia, 1996.
7. Hummel, D. and Redeker, G., "A New Vortex Flow Experiment for Computer Code Validation," RTO AVT Symposium on Vortex Flow and High Angle of Attack Aerodynamics, Loen, Norway, May 2001 2003.
8. 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, Elsevier Ltd., UK, 2004, pp. 163-172.
9. Eliasson, P., "Edge, a Navier-Stokes Solver for Unstructured Grids," Proceedings to Finite Volumes for Complex Applications III, 2002, pp. 527-534.
10. Hellsten, A., New Two-Equation Turbulence Model for Aerodynamics Applications, Ph.D. thesis, Department of Mechanical Engineering, Helsinki University of Technology (Espoo, Finland), 2004.
11. Wallin, S. and Johansson, A. V., "An Explicit and Algebraic Reynolds Stress Model for incompressible and Compressible Turbulent Flows," Journal of Fluid Mechanics, Vol. 403, 2000, pp. 89-132.
12. th International Conference on Numerical Grid Generation in Computational Field Simulation, 1998, pp. 391-400.
13. Le Moigne, Y., "Adaptive Mesh Refinement and Simulations of Unsteady Delta-Wing Aerodynamics," European Congress on Computational Methods in Applied Sciences and Engineering, ECCOMAS, 2004.
14. Tysell, L., "An Advancing Front Grid Generation System for 3D Unstructured Grids," ICAS-94-2.5.1, 1994, pp. 1552-1564.
15. 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," RTO/AVT Symposium on Vortex Flows and High Angle of Attack, Loen, Norway, May 2001.
16. th Fluid Dynamics Conference, New Orleans, LA, June 1996.