A new forced oscillation capability for the transonic dynamics tunnel

40th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2002, Pages

  Piatak, David J ^a   Cleckner, Craig S ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84894372322     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

1. Edwards, J.W. and Malone, J.B., "Current Status of Computational Methods for Transonic Unsteady Aerodynamic and Aeroelastic Applications. AGARD Structures and Materials Panel Specialist's Meeting on Transonic Unsteady Aerodynamics and Aeroelasticity. San Diego, CA, Oct. 1991.
2. Bennett, R.M., Dansberry, B.E., Farmer, M.G., Eckstrom, C.V., Seidel, D.A., Rivera, J.A., "Transonic Shock-Induced Dynamics of a Flexible Wing with a Thick Circular-Arc Airfoil". NASA TM-104088, May 1991.
3. Nixon, D., "Unsteady Transonic Aerodynamics". Vol. 120, Progress in Astronautics and Aeronautics, AIAA, Washington, D.C., 1989.
4. Rainey, A.G., "Measurement of Aerodynamic Forces for Various Mean Angles of Attack on an Airfoil Oscillating in Pitch and on Two Finite-Span Wings Oscillating in Bending with Emphasis on Damping in the Stall". NACA Technical Note 3643, May 1956.
5. Davis, S.S., Malcolm, G.N., "Experiments in Unsteady Transonic Flow". AIAA Paper 79-0769.
6. Davis, S.S., Malcolm, G.N., "Experimental Unsteady Aerodynamics of Conventional and Supercritical Airfoils". NASA TM-81221, Aug. 1980.
7. Ricketts, R.H., Sandford, M.C., Seidel, D.A., and Watson, J.J., "Transonic Pressure Distributions on a Rectangular Supercritical Wing Oscillating in Pitch". AIAA Journal of Aircraft, Vol. 21, No. 8, Aug. 1984.
8. Cunningham, A. M., Jr. and den Boer, Ruud D., "Overview of Unsteady Transonic Wind Tunnel Test on a Semispan Straked Delta Wing Oscillating in Pitch". Wright Laboratory, Flight Dynamics Directorate, WL-TR-94-3017, Aug. 1994.
9. Bennett, R.M., Eckstrom, C.V., Rivera, J.A., Dansberry, B.E., Farmer, M.G., Durham, M.H., "The Benchmark Aeroelastic Models Program-Description and Highlights of Initial Results". NASA TM-104180, December, 1991.
10. Dansberry, B.E., Durham, M.H., Bennett, R.M., Rivera, J.A. Silva, W.A., and Wieseman, C.D. "Experimental Unsteady Pressures at Flutter on the Supercritical Wing Benchmark Model". Presented at the AIAA/ASME/ASCE/AHS/ASC 34th Structures, Structural Dynamics, and Materials Conference. La Jolla, California, April, 1993.
11. Rivera, J.A., Dansberry, B.E., Bennett, R.M., Durham, M.H., and Silva, W.A., "NACA0012 Benchmark Model Experimental Flutter Results with Unsteady Pressure Distributions". NASA TM-107581, March, 1992.
12. Cole, S.R. and Garcia, J.L., "Past, Present, and Future Capabilities of the Transonic Dynamics Tunnel from an Aeroelasticity Perspective". Presented at the AIAA Dynamics Specialists Conference, Atlanta, GA, April 5-6, 2000.