SACCON static wind tunnel tests at DNW-NWB and 14′×22′ NASALaRC

28th AIAA Applied Aerodynamics Conference

Volumn 1, Issue , 2010, Pages

  Loeser, Thomas D ^a,d   Vicroy, Dan D ^b,e   Schütte, Andreas ^c  

^a German Dutch Wind Tunnels   (Germany)

^b NASA LANGLEY RESEARCH CENTER   (United States)

^c GERMAN AEROSPACE CENTER DLR   (Germany)

^d DNW NWB   (Germany)

^e NASA LaRC   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

UNDERWATER CONSTRUCTION;

DYNAMIC TESTS; INTERNATIONAL CO; NUMERICAL INVESTIGATIONS; PREDICTION METHODS; STABILITY AND CONTROL; STATIC FORCES; STATIC WIND TUNNELS; WIND TUNNEL EXPERIMENT;

WIND TUNNELS;

EID: 78649496696     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2010-4393     Document Type: Conference Paper

References (20)

1. Schütte, A.; Cummings, R.; Loeser, T.; and Vicroy, D.: "Integrated Computational/Experimental Approach to UCAV and Delta-Canard Configurations Regarding Stability & Control," 4th Symposium on Integrating CFD and Experiments in Aerodynamics, Von Karman Institute, Rhode-Saint-Genèse, Belgium, September 14-16, 2009.
2. Cummings, R.; and Schiitte, A.: "Computational/Experimental Approach to UCAV Stability & Control Estimation: Overview of NATO RTO AVT-161," AIAA-2010-4392, 28th AIAA Applied Aerodynamics Conference, Chicago, IL, June 28-July 1, 2010.
3. Schiitte, A.; Loeser, T.; and Oehlke, M.: "Prediction of the Flow Around the X-31 Aircraft Using Two Different CFD Methods," AIAA-2010-4692, 28th AIAA Applied Aerodynamics Conference, Chicago, IL, June 28 - July 1, 2010.
4. Jirasek, A.; and Cummings, R.: "Reduced Order Modeling of X-31 Wind Tunnel Model Aerodynamic Loads," AIAA-2010-4693, 28th AIAA Applied Aerodynamics Conference, Chicago, IL, June 28 - July 1, 2010.
5. Tomac, M.; and Rizzi, A.: "Comparing & Benchmarking Engineering Methods on the Prediction of X-31 Flying Qualities," AIAA-2010-4694, 28th AIAA Applied Aerodynamics Conference, Chicago, IL, June 28 - July 1, 2010.
6. Vicroy, D.; Loeser, T. and Schütte, A.: "SACCON Forced Oscillation Tests at DNW-NWB and NASA Langley 14×22-foot Tunnel" AIAA-2010-4394, 28th AIAA Applied Aerodynamics Conference, Chicago, IL, June 28 - July 1, 2010.
7. Kausche, G. et al., "The Low-Speed Wind Tunnel at DFVLR in Brunswick (Status 1988)", DFVLR-Mitt. 88-25 (1988)
8. Loeser, T., Bergmann, A., "Development of the Dynamic Wind Tunnel Testing Capabilities at DNW-NWB". AIAA-2003-453
9. Bergmann, A. et al. "Experimental and Numerical Research on the Aerodynamics of Unsteady Moving Aircraft". In: Progress in Aerospace Sciences, Elsevier, Vol. 44 (2008)
10. Hübner, A., "Experimental and Numerical Investigations of Unsteady Aerodynamic Derivatives for Transport Aircraft Configurations". AIAA-2007-1076.
11. Owens, D. B.; Brandon, J. M.; Fremaux, C. M.; Heim, E. H.; Vicroy, D. D.: "Overview of Dynamic Test Techniques for Flight Dynamic Research at NASA LaRC," AIAA-2006-3146, 25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, San Francisco, California, June 5-8, 2006.
12. Gilliot, A.: "Static and Dynamic SACCON PIV Tests - Part I: Forward Flow Field," AIAA-2010-4395, 28th AIAA Applied Aerodynamics Conference, Chicago, IL, June 28 - July 1, 2010.
13. Konrath, R.; Roosenboom, E.; Schröder, A.; Pallek, D.; and Otter, D.: "Static and Dynamic SACCON PIV Tests - Part II: Aft Flow Field," AIAA-2010-4396, 28th AIAA Applied Aerodynamics Conference, Chicago, IL, June 28 - July 1, 2010.
14. Loeser, T., Hübner, A., "Influence of Wing Elasticity on Dynamic Derivatives of Transport Aircraft". AIAA-2010-398
15. Nyland, T.W., Englund, D.R., Anderson, R.C., "On The Dynamics of short Pressure Probes: Some Design Factors Affecting Frequency Response". NASA TN D-6151 (1971)
16. de Groot; K.: Recent Results of Infrared Thermography in Wind Tunnel Tests", ONERA/DLR meeting MOTAR, Berlin, 2006.
17. Fey, U.; de Groot, K.; Le Sant, Y. "Thermography as a Tool in Wind Tunnel Testing", European Windtunnel Association (EWA), ANE3-CT-2004-502889, Network of Excellence, Priority 4, Aeronautics and space, Deliverable 2.10.
18. AGARDograph 109 "Subsonic Wind Tunnel Wall Corrections", October 1966
19. Eckert, D.: "Wall Correction Formulae for on-line Processing of Measurements with Conventional Aircraft Models at DNW". DNW-PA-88.018.
20. Schuette, A.; Hummel, D.; Hitzel, S.: "Numerical and Experimental Analyses of the Vortical Flow Around the SACCON Configuration", AIAA-2010-1400, 28th AIAA Applied Aerodynamics Conference, Chicago, IL, June 28 - July 1, 2010.