Analysis of PIV results obtained for the VFE-2 65° delta wing configuration at sub- And transonic speeds

Collection of Technical Papers - AIAA Applied Aerodynamics Conference

Volumn 2, Issue , 2006, Pages 746-760

  Konrath, Robert ^a   Schröder, Andreas ^a   Kompenhans, Jürgen ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE MEASUREMENT; CODES (SYMBOLS); REYNOLDS NUMBER; TRANSONIC AERODYNAMICS; VELOCITY MEASUREMENT; VORTEX FLOW; WIND TUNNELS;

PARTICLE IMAGE VELOCIMETRY (PIV); SWEEP ANGLES; VORTEX BREAKDOWN;

DELTA WING AIRCRAFT;

EID: 33845428022     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-3003     Document Type: Conference Paper

References (10)

1. 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, 7-11 May 2001, Meeting Proceedings RTO-MP-069 (I), SYA 8-1 to 8-31, 2003
2. 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
3. Klein, C., Sachs, W., Henne, U., Engler, R.H., Wiedemarm, 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
4. Konrath, R., Klein, C., Engler, R.H., Otter, D., "Analysis of PSP Results Obtained for the VFE-2 65° Delta Wing Configuration at Sub- and Transonic Speed," AIAA-Paper 2006-0060, 2006
5. Schröder, A., Agocs, J., Frahnert, H., Otter, D., Mattner, H., Kompenhans, J., Konrath, R., "Application of Stereo PIV to the VFE-2 65° Delta Wing Configuration at Sub- and Transonic Speeds", AIAA-Paper 2006-3486, 2006
6. Luckring, J.M., "Compressibility and leading-edge bluntness effects for a 65° delta-wing," AIAA Paper 2004-0765, 2004
7. Luckring, J.M., "Reynolds number, compressibility, and leading-edge bluntness effects on delta-wing aerodynamics," ICAS Proceedings, Paper 4.1.4., 2004
8. Hummel, D., "Effects of Boundary Layer Formation on the Vortical Flow above Slender Delta Wings," RTO Specialists' Meeting on Enhancement of NATO Military Flight Vehicle Performance by Management of Interacting Boundary Layer Transition and Separation, Prague, Czech Republic, 4-7 October 2004, Meeting Proceedings RTO-MP-AVT-111, pp. 30-1 to 30-22, 2004
9. nd International Symposium on Integrating CFD and Experiments in Aerodynamics, Cranfield University (Shrivenham), UK, 5-6 September, pp. 1-12, 2005
10. Schiavetta, L., Boelens, O., Fritz, W., "Analysis of Transonic Flow on a Slender Delta Wing Using CFD," AIAA-Paper 2006-3171, 2006