Development of PSP technique for application on the VFE- 2 65° delta wing configuration

Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting

Volumn 2, Issue , 2006, Pages 764-776

  Klein, Christian ^a   Sachs, Werner E ^a   Henne, Ulrich ^a   Engler, Rolf H ^a   Wiedemann, Andreas ^a   Konrath, Robert ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

CCD CAMERAS; NASA; PRESSURE MEASUREMENT; PRESSURE SENSORS; TRANSONIC AERODYNAMICS; WIND TUNNELS;

DELTA-WING MODEL; DLR'S MOBILE PSP SYSTEM; FLOW TOPOLOGY; PLANAR PRESSURE; PRESSURE TAPS;

VORTEX FLOW;

EID: 34250763157     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-59     Document Type: Conference Paper

References (8)

1. Hummel, D. & 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-068 (I), SYA 8-1 to 8-31, (2003).
2. Chu, J. & Luckring, J.M., "Experimental surface pressure data obtained on 65° delta wing across Reynolds number and Mach number ranges", NASA TM 4645, (1996).
3. Engler, R. H., Hartmann, K., Troyanovski, I. & Vollan, A., "Description and assessment of a new optical pressure measurement system (OPMS) demonstrated in the high speed wind runnel of DLR in (Göttingen) ", DLR FB 92 24, (1992).
4. Vollan, A. & Alati, L., "A New Optical Pressure Measurement System", 14th ICIASF Congress, Rockville, MD, (1991).
5. Engler, R.H. & Klein, Chr., "First Results Using the New DLR PSP System -Intensity and Lifetime Measurements", Conference Wind Tunnels and Wind Tunnel Test Techniques, Cambridge UK, ISBN 185768 048 0, (1997).
6. Morris, M.J., Donovan, J.F., Kegelmann, J.T., Schwab, S.D., Levy, R.L. & Crites, R.C., "Aerodynamic Applications of Pressure Sensitive Paint", AIAA Journal, Vol. 31, No.3, 419-425, (1993).
7. Konrath, R., Klein, Chr., Engler, R.H. & Otter, D., "Analysis of PSP Results Obtained for the VFE-2 65° Delta Wing Configuration at Sub- and Transonic Speeds", AIAA-Paper 2006-0060, (2006).
8. nd International Symposium on Integrating CFD and Experiments in Aerodynamics", Cranfield University (Shrivenham), UK, 5-6 September, pp. 1-12, (2005).