Benchmark active controls technology model aerodynamic data

Journal of Guidance, Control, and Dynamics

Volumn 23, Issue 5, 2000, Pages 914-921

  Scott, Robert C ^a   Hoadley, Sherwood T ^a   Wieseman, Carol D ^a   Durham, Michael H ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOADS; COMPUTATIONAL FLUID DYNAMICS; CONTROL SYSTEM ANALYSIS; CONTROL SYSTEM SYNTHESIS; FLUTTER (AERODYNAMICS); MATHEMATICAL MODELS; UNSTEADY FLOW; WIND TUNNELS;

BENCHMARK ACTIVE CONTROL SYSTEMS;

WINGS;

EID: 0034275786     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.4632     Document Type: Article

References (9)

1. Rivera, J. A., Jr., Dansberry, B. E., Farmer, M. G., Eckstrom, C. V., Seidel, D. A., and Bennett, R. M., "Experimental Flutter Results with Steady and Unsteady Pressure Measurements of a Rigid Wing on a Flexible Mount System," AIAA Paper 91-1010, April 1991.
2. Durham, M. H., Keller, D. F., Bennett, R. M., and Wieseman, C. D., "A Status Report on a Model for Benchmark Active Controls Testing," AIAA Paper 91-1011, April 1991.
3. Waszak, M. R., "Parameter Estimation and Analysis of Actuators for the BACT Wind-Tunnel Model," AIAA 96-3362, 1996.
4. Farmer, M. G., "A Two-Degree-of-Freedom Flutter Mount System with Low Damping for Testing Rigid Wings at Different Angles of Attack," NASA TM 83302, 1982.
5. "The Langley Transonic Dynamics Tunnel," NASA Langley Research Center Working Paper LWP-799, Sept. 1969.
6. Pototzky, A. S., Wieseman, C. D., Hoadley, S. T., and Mukhopadhyay, V., "On-Line Performance Evaluation of Multi-Loop Digital Control Systems," Journal of Guidance, Control, and Dynamics, Vol. 15, No. 4, 1992, pp. 878-884.
7. Wieseman, C. D., and Hoadley, S. T., "Versatile Software Package for Near Real-Time Analysis of Experimental Data," AIAA Paper 98-2722, June 1998.
8. Rivera, J. A., Jr., Dansberry, B. E., Bennett, R. M., Durham, M. H., and Silva, W. A., "NACA 0012 Benchmark Model Experimental Flutter Results with Unsteady Pressure Distributions," NASA TM 107581, March 1992.
9. Waszak, M. R., "Modeling the Benchmark Active Control Technology Wind-Tunnel Model for Application to Flutter Suppression," AIAA Paper 96-3437, July 1996.