Activities in aeroelasticity at NASA Langley Research Center

American Society of Mechanical Engineers, Aerospace Division (Publication) AD

Volumn 53, Issue , 1997, Pages 77-88

  Perry III, Boyd ^a   Noll, Thomas E ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DATA ACQUISITION; ENGINEERING RESEARCH; WIND TUNNELS;

LANGLEY TRANSONIC DYNAMICS TUNNEL;

AERODYNAMICS;

EID: 0031360965     PISSN: 07334230     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Article

References (16)

1. Edwards, J., "Transonic Shock Oscillations Calculated with a New Interactive Boundary Layer Coupling Method," AIAA Paper 93-0777, January 1993.
2. Edwards, J., "Transonic Shock Oscillations and Wing Flutter Calculated with an Interactive Boundary Layer Method," Proceedings of the EUROMECH-Colloquium 349, Simulation of Fluid-Structure Interaction in Aeronautics, Gottingen, Germany, September 1996.
3. Gibbons, M., "Aeroelastic Calculations Using CFD for a Typical Business Jet Model," NASA CR 4753, September 1996.
4. Johnson, W.: "A Comprehensive Analytical Model of Rotorcraft Aerodynamics and Dynamics." NASA TM-81182, 1980.
5. Kvaternik, R., "Studies in Tilt-Rotor VTOL Aircraft Aeroelasticity," PhD Dissertation from Case Western Reserve University, June 1973.
6. Lichtenwalner, P., Little, G., and Scott, R., "Adaptive Neural Control of Aeroelastic Response," Proceedings of the 37th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Salt Lake City, UT, April 1996.
7. McGowan, A., Heeg, J, and Lake, R., "Results from Wind-Tunnel Testing from the Piezoelectric Aeroelastic Response Tailoring Investigation," Proceedings of the 37th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Salt Lake City, UT, April 1996.
8. Moses, R., "Active Vertical Tail Buffeting Alleviation on a Twin-Tail Fighter Configuration in a Wind Tunnel," Proceedings of the CEAS International Forum on Aeroelasticity and Structural Dynamics, Rome, Italy, June 1997.
9. Nixon, M. W., "Aeroelastic Response and Stability of Tiltrotors with Elastically-Coupled Composite Rotor Blades," PhD Dissertation from the University of Maryland, December 1993.
10. Nixon, M. W., Kvaternik, R. G., and Settle, T. B., "Tiltrotor Vibration Reduction Through Higher Harmonic Control," Proceedings of the CEAS International Forum on Aeroelasticity and Structural Dynamics, Rome, Italy, June 1997.
11. Scott, R. C. Wieseman, C. D., Hoadley, S. T., and Durham, M. H., "The Benchmark Active Controls Technology Model Aerodynamic Data," Proceedings of the AIAA 35th Aerospace Sciences Meeting and Exhibit, Reno, NV, January 1997.
12. Silva, W., "Application of Nonlinear Systems Theory to Transonic Unsteady Aerodynamic Responses," AIAA Journal of Aircraft, Volume 30, Number 5, September-October 1993, pps 660-668.
13. Silva, W., "Extension of Nonlinear Systems Theory to General-Frequency Unsteady Transonic Aerodynamic Responses," AIAA Paper No. 93-1590, Presented at the 34th Structures, Structural Dynamics, and Materials Conference, La Jolla, CA, April 19-21, 1993.
14. Staff of the Aeroelasticity Branch, "The Transonic Dynamics Tunnel," Langley Working Paper 799, July 1992.
15. Theodorsen, Theodore, "General Theory of Aerodynamic Instability and the Mechanism of Flutter," NACA Report 496, 1935.
16. Wilkie, W. K., Belvin, W. K., and Park, K. C, "Aeroelastic Analysis of Helicopter Rotor Blades Incorporating Anisotropic Piezoelectric Twist Actuation," AD-Vol. 52, Proceedings of the ASME Aerospace Division, November, 1996, pp. 423-433.