Active warping control of a joined-wing airplane configuration

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

Volumn 4, Issue , 2003, Pages 2847-2861

  Cesnik, Carlos E S ^a   Brown, Eric L ^b  

^a UNIVERSITY OF MICHIGAN   (United States)

^b MASSACHUSETTS INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AIRCRAFT; COMPUTER SIMULATION; DEFLECTION (STRUCTURES); ELECTRIC FIELD EFFECTS; FINITE ELEMENT METHOD; MANEUVERABILITY; PIEZOELECTRIC MATERIALS; STRAIN RATE; SUBSONIC AERODYNAMICS;

ACTIVE WARPING CONTROL; FINITE STATE UNSTEADY SUBSONIC AIRLOADS; JOINED WING AIRPLANE CONFUIGURATION;

WINGS;

EID: 0042511908     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

1. Pendleton, E. W., Griffin, K. E., Kehoe, M., and Perry, B., "A Flight Research Program for the Active Aeroelastic Wing Concept," In Proceedings of the 37th AIAA/ASME/AHS/ASC Structures, Structural Dynamics and Materials Conference, Salt Lake City, Utah, April 1996.
2. Bent, A. A., "Active Fiber Composite Material Systems for Structural Control Applications," In Proceedings of the SPIE's 6th International Symposium on Smart Structures and Materials, Newport Beach, California, March 1999.
3. Wilkie, W.K., Bryant, R.G., High, J.W., Fox, R.L., Hellbaum, R.F., Jalink, A., Little, B.D., and Mirick, P.H., "Low-cost piezocomposite actuator for structural control applications," In Proceedings of the SPIE 7th Symposium on Smart Structures and Materials, Newport Beach, California, March 2000. pp. 323-334.
4. Cesnik, C. E. S. and Ortega-Morales, M., "Active Aeroelastic Tailoring of Slender Flexible Wings," International Forum on Aeroelasticity and Structural Dynamics, Madrid, Spain, June 5-7, 2001.
5. Brown, E. L., "Integrated Strain Actuation in Aircraft with Highly Flexible Composite Wings," Ph.D. Thesis, Massachusetts Institute of Technology, Cambridge, Massachusetts, June 2003.
6. Livne, E., "Aeroelasticity of Joined-Wing Airplane Configurations: Past Work and Future Challenges - A Survey," In Proceedings of the 42nd AIAA/ASME/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Seattle, WA, April 16-19, 2001, AIAA-2001-1370.
7. Blair, M. and Canfield, R. A., "A Joined-Wing Structural Weight Modeling Study," In Proceedings of the 43rd AIAA/ASME/AHS/ASC Structures, Structural Dynamics and Materials Conference, Denver, Colorado, April 2002, AIAA-2002-1337.
8. Roberts, R. W., Canfield, R. A., and Blair, M., "Sensor-craft Structural Optimization and Analytical Certification," In Proceedings of the 44th AIAA/ASME/AHS/ASC Structures, Structural Dynamics and Materials Conference, Denver, Colorado, April 2003.
9. Reich, G. W., Raveh, D., and Zink, P. S., "Application of Active Aeroelastic Wing Technology to a Joined-Wing Sensorcraft," In Proceedings of the 43rd AIAA/ASME/AHS/ASC Structures, Structural Dynamics and Materials Conference, Denver, Colorado, April 2002, AIAA-2002-1633.
10. Peters, D. A. and Johnson, M. J. "Finite-State Airloads for Deformable Airfoils on Fixed and Rotating Wings", In Symposium on Aeroelasticity and Fluid/Structure Interaction, Proceedings of the Winter Annual Meeting. ASME, November 6-11, 1994.
11. Ikegami, R., Private communication. The Boeing Co., Phantom Works, Seattle, Washington, 2002.
12. Rossetti, Jr., G. A., Pizzochero, A., and Bent, A. A., "Recent Advances in Active Fiber Composites Technology," In Proceedings of the 12th IEEE International Symposium on Applications of Ferroelectrics, Honolulu, Hawaii, 2000, pp. 753-756.