Modeling the benchmark active control technology windtunnel model for application to flutter suppression

21st Atmospheric Flight Mechanics Conference

Volumn , Issue , 1996, Pages 632-643

  Waszak, Martin R ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTICITY; BENCHMARKING; CONTROLLERS; EQUATIONS OF MOTION; FLUTTER (AERODYNAMICS); FREQUENCY RESPONSE;

AEROELASTIC RESPONSE; BENCHMARK ACTIVE CONTROL TECHNOLOGIES; DESIGN AND ANALYSIS; EXPERIMENT AND ANALYSIS; EXPERIMENTAL FREQUENCIES; LAGRANGE'S EQUATION; PRINCIPLE OF VIRTUAL WORK; WIND TUNNEL MODELING;

WIND TUNNELS;

EID: 84983165302     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-3437     Document Type: Conference Paper

References (12)

1. 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 No. 91-1011.
2. Bennett. R. M.; Eckstrom, C. V.; et al.: The Benchmark Aeroelastic Models Program-Description and Highlights of Initial Results. NASA TM-104180, Dec. 1991.
3. Wieseman, C. D.; Hoadley, S. T.; and McGraw, S. M.: On-Line Analysis Capabilities Developed to Support Active Flexible Wing Wind-Tunnel Model. Journal of Aircraft. Vol. 23, No. 1. pp. 39-44. Jan.-Feb. 1995.
4. Adams, W. M.: ISAC: A Tool for Aeroservoelastic Modeling and Analysis. NASA TM-109031. December, 1993.
5. Rivera, Jr., J. A.; Dansberry, B. E.; et al.: NACA 0012 Benchmark Model Experimental Flutter Results with Unsteady Pressure Distributions. AIAA Paper No. 92-2396. 33rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Dallas, TX, April 1992.
6. Baals, D. D. and Corliss, W. R.: Wind Tunnels of NASA. pp. 79-81. NASA SP-440.
7. Rivera, Jr., J. A.; Dansberry, B. E.; Durham, M. H.; Bennett, R. M.; and Silva, W. A.: Pressure Measurements on a Rectangular Wing with a NACA 0012 Airfoil During Conventional Flutter. NASA TM-104211, July 1992.
8. Bisplinghoff, R. L. and Ashley, H.: Principles of Aeroelasticity. Dover Publications, Inc., New York. 1962.
9. Waszak, M. R. and Schmidt, D. K.: Flight Dynamics of Aeroelastic Vehicles. Journal of Aircraft, pp. 563-571. Vol. 25, No 6. June 1988.
10. Dansberry, B. E.; Durham, M. H.; Bennett, R. M.; Turnock, D. L.; Silva, W. A.; and Rivera, Jr., J. A.: Physical Properties of the Benchmark Models Program Supercritical Wing. NASA TM-4457. September 1993.
11. Waszak, M. R. and Fung, J.: Parameter Estimation and Analysis of Actuators for the BACT Wind-Tunnel Model. AIAA Paper No. 96-3362. AIAA Atmospheric Flight Mechanics Conference. San Diego, CA. July 29-31, 1996.
12. Sleeper, R. K.; Keller, D. F.; Perry III, B.; and Sanford, M. C.: Characteristics of Vertical and Lateral Tunnel Turbulence Measured in Air in the Langley Transonic Dynamics Tunnel. NASA TM-107734. March 1993.