Contributions of the NASA Langley research center to the DARPA/AFRL/NASA/Northrop Grumman smart wing program

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 7, Issue , 2003, Pages 5106-5124

  Florance, Jennifer P ^a   Burner, Alpheus W ^a   Fleming, Gary A ^a   Hunter, Craig A ^a   Graves, Sharon S ^a   Martin, Christopher A ^b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b NORTHROP GRUMMAN CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MODELS; COMPUTATIONAL FLUID DYNAMICS; FIGHTER AIRCRAFT; FLIGHT DYNAMICS; INTERFEROMETRY; NAVIER STOKES EQUATIONS; PHOTOGRAMMETRY; REYNOLDS NUMBER; TRANSONIC AERODYNAMICS; WIND TUNNELS;

LANGLEY RESEARCH CENTER; PROJECTION MOIRE INTERFEROMETRY; TRANSONIC DYNAMICS TUNNEL; UNMANNED COMBAT AIR VEHICLE; VIDEOGRAMMETRIC MODEL DEFORMATION;

WINGS;

EID: 0041464934     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (19)

1. Smart Materials and Structures - Smart Wing Phase 1, Volumes I, II, III, and IV, Contract Final Report, AFRL-ML-WP-TR-1999-4162, Contract Number F33615-95-C-3202, December 1998.
2. Kudva, Jayanth N.; Martin, Christopher A.; Scherer, Lewis B.; Jardine, A. Peter; McGowan, Anna-Maria Rivas; Lake Renee C.; Sendeckyj, George P.; Sanders, Brian P., "Overview of the DARPA/AFRL/NASA Smart Wing program", SPIE Conference on Smart Structures and Materials, Industrial and Commercial Applications of Smart Structures Technologies, Paper #3674-26, pp. 230-236, July 1999.
3. Kudva, J. N.; Sanders, B.; Pinkerton-Florance, J.; Garcia, E., "Overview of the DARPA/AFRL/NASA Smart Wing Phase 2 Program", SPIE Conference on Smart Structures and Materials, Industrial and Commercial Applications of Smart Structures Technologies, Paper #4332-48, pp 383-389, June 2001.
4. Martin, C. A.; et al, "Design, Fabrication and Testing of the Scaled Wind Tunnel Model for the Smart Wing Phase 2 Program", SPIE's 9th Annual Symposium on Smart Structures and Materials, Paper #4698-05, pp 44-52, July 2002.
5. Bartley-Cho, Jonathan D.; Wang, D. P.; West, Mark N., "Development, Control, and Test Results of High Rate, Hingeless Trailing Edge Control Surface for the Smart Wing Phase 2 Wind Tunnel Model", SPIE's 9th Annual Symposium on Smart Structures and Materials, Paper #4698-06, pp 53-63, July 2002.
6. Kudva, J.N.; Sanders, B.; Pinkerton-Florance, J.; Garcia, E., "DARPA/AFRL/NASA Smart Wing Program: Final Overview", SPIE's 9th Annual Symposium on Smart Structures and Materials, Paper #4698-04, pp 37-43, July 2002.
7. Scherer, L. B.; et al, "DARPA/AFRL Smart Wing Phase 2 Wind Tunnel Test Results", SPIE's 9th Annual Symposium on Smart Structures and Materials, Volume 4698, Paper #4698-07, pp 64-75, July 2002.
8. Smart Materials and Structures - Smart Wing Phase 2, Contract Final Report, Contract Number F33615-97-C-3213, Expected Publication July 2003.
9. The NASA Langley Transonic Dynamics Tunnel, LWP-799, September 1969.
10. Burner, A. W.; Liu, Tianshu, "Videogrammetric Model Deformation Measurement Technique", Journal of Aircraft, Vol. 38, No. 4, pp. 745-754, July-August, 2001.
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13. Martin, C. A.; Scherer, L. B.; West, M. N.; Florance, J.; Wieseman, C.; Burner, A. W.; Fleming, G. A., "DARPA/ARFL/NASA Smart Wing second wind tunnel test results", SPIE's 6th Annual International Symposium on Smart Structures and Materials, Industrial and Commercial Applications of Smart Structures Technologies, Paper #3674-28, March 1-5, 1999.
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