Wing deformation measurements of the DLR-F6 Transport Configuration in the National Transonic Facility

Collection of Technical Papers - AIAA Applied Aerodynamics Conference

Volumn , Issue , 2008, Pages

  Burner, Alpheus W ^a,b,c   Goad, William K ^a,b   Massey, Edward A ^a,b   Goad, Linda R ^a,c   Goodliff, Scott L ^a,b,c   Bissen, Owen W ^a,b,c  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b M S 267

^c AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

DEFORMATION; PHOTOGRAMMETRY; REYNOLDS NUMBER; SUPERSONIC AIRCRAFT; TRANSONIC AERODYNAMICS;

AERODYNAMIC LOADING; EXPERIMENTAL TECHNIQUES; INDEPENDENT MEASUREMENT; LIFT COEFFICIENT; PHOTOGRAMMETRIC TECHNIQUE; STATIC EXPERIMENTS; STEREOPHOTOGRAMMETRY; WING DEFORMATION;

LIFT;

EID: 85067321984     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-6921     Document Type: Conference Paper

References (13)

1. Burner, A. W.; Wahls, R. A.; and Goad, W. K., "Wing Twist Measurements at the National Transonic Facility," NASA TM 110229 1996.
2. Burner, A. W. and Liu, T., "Videogrammetric Model Deformation Measurement Technique," Journal of Aircraft, Vol. 38, No. 4, 2001, pp. 745-754.
3. Spain, C. V., Heeg, J., Ivanco, T. G., Barrows, D. A., Florence, J. R., Burner, A. W., DeMoss, J., Lively, P. S., "Assessing Videogrammetry for Static Aeroelastic Testing of a Wind-Tunnel Model," AIAA-2004-1677, 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, April 2004.
4. Barrows, D. A., Burner, A. W., Berry, F. C., Dismond, H. R. and Cate, K. H., "Photogrammetric Measurements of CEV Airbag Landing Attenuation Systems," AIAA-2008-846, 46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 7-10, 2008.
5. Burner, A. W., Lokos, W. A., Barrows, D. A., "Aeroelastic Deformation: Adaptation of Wind Tunnel Measurement Concepts to Full-Scale Vehicle Flight Testing," RTO-MP-AVT-124; RTO/AVT-123 Symposium on Flow Induced Unsteady Loads and the Impact on Military Applications, Budapest, Hungary, 25-29 Apr. 2005.
6. Hooker, J. R., Burner, A. W., Valla, R., "Static Aeroelastic Analysis of Transonic Wind Tunnel Models using Finite Element Methods," AIAA 97-2243, 15th AIAA Applied Aerodynamics Conference, June 23-25, 1997.
7. Gatlin, G. M., Rivers, M. B., Goodliff, S. L., Rudnik, R., and Sitzmann, M., "Experimental Investigation of the DLR-F6 Transport Configuration in the National Transonic Facility," AIAA 2008-6917, August 2008.
8. Vassberg, J. C., Tinoco, E. N., Mani, M., Brodersen, O. P., Eisfeld, B., Wahls, R. A., Morrison, J. H., Zickuhr, T., Laflin, K. R., and Mavriplis, D. J., "Abridged Summary of the Third AIAA Computational Fluid Dynamics Drag Prediction Workshop," Journal of Aircraft Vol.45, No.3, 2008, pp. 781-798.
9. Keye, S., and Rudnik, R., "Static Aero-Elastic Simulation of DLR's F6 Wing-Body Configuration and Comparison to Experimental Data," accepted for the 47th AIAA Aerospace Sciences Meeting, Orlando, Florida, 5-8 Jan 2009.
10. Rossow, C. C., Godard, J. L., Hoheisel, H., and Schmitt, V., "Investigation of Propulsion Integration Interference on a Transport Aircraft Configuration," AIAA 92-3097, 1992.
11. Burner, A. W., and Barrows, D. A., "Error Due to Wing Bending in Single-Camera Photogrammetric Technique," NASA TM-2005-213254, May 2005.
12. Burner, A. W., Liu, T., DeLoach, R., "Uncertainty of Videogrammetric Techniques used for Aerodynamic Testing," AIAA-2002-2794, 22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, Saint Louis, MO, June 2002.
13. Crawford, B. L., "Angle Measurement System. (AMS) for Establishing Model Pitch and Roll Zero, and Performing Single Axis Angle Comparisons," AIAA-2007-1162, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 8-11, 2007.