Static and dynamic SACCON PIV tests-part II: Aft flow field

28th AIAA Applied Aerodynamics Conference

Volumn 1, Issue , 2010, Pages

  Konrath, Robert ^a   Roosenboom, Eric W M ^a   Schröder, Andreas ^a   Pallek, Dieter ^a   Otter, Dirk ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; ANGLE OF ATTACK INDICATORS; FLIGHT CONTROL SYSTEMS; MILITARY PHOTOGRAPHY; MILITARY VEHICLES; STABILITY CRITERIA; STEREO IMAGE PROCESSING; VELOCITY; VELOCITY MEASUREMENT;

EXPERIMENTAL ANALYSIS; EXPERIMENTAL INVESTIGATIONS; HIGH RESOLUTION CAMERA; INTEGRATED DESIGNS; STABILITY AND CONTROL; STEREOSCOPIC PARTICLE IMAGE VELOCIMETRY; SYNERGETIC DESIGN; UNMANNED COMBAT AIR VEHICLES;

FLOW FIELDS;

EID: 78649517819     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2010-4396     Document Type: Conference Paper

References (18)

1. Loeser, T., Vicroy, D., and Schuette, A., "SACCON Static Wind Tunnel Tests at DNW-NWB and 14'×22' NASA LaRC (AIAA Paper 2010-4393)," 28th AIAA Applied Aerodynamics Conference, Chicago, II, June-July 2010.
2. Vicroy, D., and Loeser, T., "SACCON Dynamic Wind Tunnel Tests at DNW-NWB and 14'×22' NASA LaRC (AIAA Paper 2010-4394)," 28th AIAA Applied Aerodynamics Conference, Chicago, II, June-July 2010.
3. Schütte A., Cummings, R.M., Loeser, T., and Vicroy, D.D., "Integrated Computational/Experimental Approach to UCAV and Delta-Canard Configurations Regarding Stability & Control," 4th Symposium on Integrating CFD and Experiments in Aerodynamics, Rhode-Saint-Genèse, Belgium, 2009.
4. Cummings, R.M., and Schütte A., "An Integrated Computational/Experimental Approach to UCAV Stability & Control Estimation: Overview of NATO RTO AVT- 161 (AIAA Paper 2010-4392)," 28th AIAA Applied Aerodynamics Conference, Chicago, Il, June-July 2010.
5. Fujii, K., "Progress and future prospects of CFD in aerospace - Wind tunnel and beyond," Progress in Aerospace Sciences 41, 2005, pp. 455-470.
6. Oberkampf, W.L., and Trucano, T.G., "Verification and validation in computational fluid dynamics", Progress in Aerospace Sciences 38, 2002, pp. 209-272.
7. Roosenboom, E.W.M., Stürmer, A., and Schröder, A., "Advanced experimental and numerical validation and analysis of propeller slipstream flows," Journal of Aircraft, Vol. 47, No. 1, 2010, pp. 284-291.
8. Gursul, I., "Vortex flows on UAVs: Issues and challenges," The Aeronautical Journal, 2004, pp. 597-610.
9. Hall, M.G., "Vortex breakdown," Annual Review of Fluid Mechanics (4), 1972, pp. 195-218.
10. Leibovich, S., "Vortex Stability and Breakdown: Survey and Extension," ALAA Journal (22) 9, 1983, pp 1192-1206.
11. Goruney, T., and Rockwell, D., Ëffect of Pitch Rate on Near-Surface Topology on a Delta Wing," AIAA Journal (48) 6, 2010, pp. 1207-1220.
12. Gilliot, A., Morgand, S., Monnier, J.C., Le Roy, J.F., Geiler, C., and Pruvost, J., "Static and Dynamic SACCON PIV Tests-Part I: Forward Flowfield (AIAA Paper 2010-4395)," 28th AIAA Applied Aerodynamics Conference, Chicago, II, June-July 2010.
13. Bergmann, A.; Hübner, A., and Loeser, T., "Experimental and numerical research on the aerodynamics of unsteady moving aircraft," Progress in Aerospace Sciences, Volume 44, Issue 2, 2008, pp. 121-137.
14. Konrath, R., Klein, C., Schröder, A., and Kompenhans, J., "Combined application of pressure sensitive paint and particle image velocimetry to the flow above a delta wing," Experiments in Fluids 44: 357-366, 2008.
15. Schütte A., Hummel D., and Hitzel S., "Numerical and experimental analyses of the vortical flow around the SACCON configuration", 28th AIAA Applied Aerodynamics Conference, Chicago, Il, June-July, AIAA Paper 2010-4690, 2010.
16. 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.
17. Luckring, J.M., "Compressibility and leading-edge bluntness effects for a 65° delta-wing," AIAA Paper 2004-0765, 2004.
18. Konrath, R., Klein, C., and Schröder, A., "PSP and PIV investigations on the VFE-2 configuration in sub- and transonic flow," AIAA-Paper 2008-379, 46th AIAA Aerospace Sciences Meeting and Exhibit January 2008, Reno, NV.