What was learned from the new VFE-2 experiments?

46th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2008, Pages

  Luckring, James M ^a   Hummel, Dietrich ^b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b TECHNICAL UNIVERSITY OF BRAUNSCHWEIG   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING;

EXPERIMENTS;

EID: 78149418296     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (27)

1. Chu, J., and Luckring, J. M., "Experimental Surface Pressure Data Obtained on 65° Delta Wing Across Reynolds Number and Mach Number Ranges, " NASA TM 4645, 1996.
2. Luckring, J. M., "Reynolds Number and Leading-Edge Bluntness Effects on a 65° Delta Wing, " AIAA Paper 2002-0419, 2002.
3. Luckring, J. M., "Transonic Reynolds Number and Leading-Edge Bluntness Effects on a 65° Delta Wing, " AIAA Paper 2003-0753, 2003.
4. Luckring, J. M., "Compressibility and Leading-Edge Bluntness Effects for a 65° Delta Wing, " AIAA Paper 2004-0765, 2004.
5. Luckring, J. M., "Reynolds Number, Compressibility, and Leading-Edge Bluntness Effects on Delta-Wing Aerodynamics, " ICAS Proceedings Yokohama 2004, Paper 4.1.4, 2004.
6. Hummel, D., and Redeker, G., "A New Vortex Flow Experiment for Computer Code Validation, " RTO AVT Symposium Vortex Flow and High Angle of Attack Aerodynamics, Loen, Norway, 7-11 May 2001, Meeting Proceedings RTO-MP-069 (I), SYA 8-1 to 8-31, 2003.
7. Hummel, D., "Review of the Second International Vortex Flow Experiment (VFE-2), " AIAA Paper 2008-0377, 2007.
8. Luckring, J. M., "Initial Experiments and Analysis of Vortex Flow on Blunt Edged Delta Wings, " AIAA Paper 2008-0378, 2007.
9. Konrath, R., Klein, Ch. and Schroeder, A., "PSP and PIV Investigations on the VFE-2 Configuration in Sub- and Transonic Flow, " AIAA Paper 2008-0379, 2007.
10. LeRoy, J. F., Rodriguez, O. and Kurun, S., "Experimental and CFD Contribution to Delta Wing Vortical Flow Understanding, " AIAA Paper 2008-0380, 2007.
11. Furman, A. and Breitsamter, Ch., "Turbulent and Unsteady Flow Characteristics of Delta Wing Vortex Systems, " AIAA Paper 2008-0381, 2007.
12. Coton, F., Mat, S. and Galbraith, R., "Low Speed Wind Tunnel Characterization of the VFE-2 Wing, " AIAA Paper 20080382, 2007.
13. Hummel, D., "Effects of Boundary Layer Formation on the Vortical Flow Above Slender Delta Wings, " RTO AVT Symposium Enhancement of NATO Military Flight Vehicle Performance by Management of Interacting Boundary Layer Transition and Separation, Prague, Czech Republic, 4-8 Oct 2004, Meeting Proceedings RTO-MP-AVT-111, 30-1 to 30-22, 2004.
14. Klein, C., Sachs, W., Henne, U., Engler, R.H., Wiedemann, A., and Konrath, R., "Development of PSP Technique for Application on the VFE-2 65° Delta Wing Configuration in Sub- and Transonic Flow, " AIAA Paper 2006-0059, 2006.
15. Konrath, R., Klein, C., Engler, R. H., and Otter, D., "Analysis of PSP Results Obtained for the VFE-2 65° Delta Wing Configuration at Subsonic and Transonic Speed, " AIAA Paper 2006-0060, 2006.
16. Fritz, W., "Numerical Simulation of the Peculiar Subsonic Flow Field about the VFE-2 Delta Wing with Rounded Leading Edge, " AIAA Paper 2008-0393, 2008.
17. Schröder, A., Agocs, J., Frahnert, H., Otter, D., Mattner, H., Kompenhans, J., and Konrath, R., "Application of Stereo-PIV to the VFE-2 65° Delta Wing Configuration at Sub- and Transonic Speeds, " AIAA Paper 2006-3486, 2006.
18. Konrath, R., Schröder, A., and Kompenhans, J., "Analysis of PIV Results Obtained for the VFE-2 65° Delta Wing Configuration at Sub- and Transonic Speeds, " AIAA Paper 2006-3003, 2006.
19. th International Symposium on Flow Visualization, Sept. 10 -14, 2006, DLR Goettingen, Germany, In Grant, I. [Ed.]: CD Rom Proceedings (ISFV12-67.2), Optimage Ltd., Edinburgh, UK, pp. 1 - 14.
20. Sheplak, M., "The Year in Review: Aerodynamic Measurement Technology, " Aerospace America, December 2006, p. 22.
21. nd International Symposium Integrating CFD and Experiments in Aerodynamics, 5 - 6 September 2005, Cranfield University, UK, J. Aerospace Engineering, Vol.. 220, 2006, Nr. 6, pp. 559 - 568.
22. Hummel, D., "The Second International Vortex Flow Experiment (VFE-2) - Objectives and Present Status, " AIAA Paper 2007-4446, 2007.
23. Furman, A. and Breitsamter, Ch., "Delta Wing Steady Pressure Investigations for Sharp and Rounded Leading Edges, " In: Rath, H.-J., Holze, C., Heinemann, H.-J., Henke, R. and Hönlinger, H. (Eds), New Results in Numerical and Experimental Fluid Mechanics V, 2004, Vol. 92 of Notes on Numerical Fluid Mechanics and Multidisciplinary Design, pp. 77 - 84.
24. Furman, A. and Breitsamter, Ch., "Investigations of Flow Phenomena on Generic Delta Wing, " ICAS Proceedings Hamburg 2006, Paper 3.1.2 (2006).
25. st CEAS Conference Berlin 2007, Paper 2007-430, 2007.
26. Visbal, M. R., "Computed Unsteady Structure of Spiral Vortex Breakdown on Delta Wings, " AIAA Paper 96-2074, 1996.
27. Müller, J., and Hummel, D., "Numerical Analysis of the Unsteady Flow Above a Slender Delta Wing at Large Angles of Attack, " ICAS Proceedings Harrogate 2000, Paper ICA0252, 2000.