Modelling and sensitivity analysis of a variable geometry trailing edge control surface

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

Volumn 5, Issue , 2003, Pages 3746-3756

  Forster, E ^a   Sanders, B ^a   Eastep, F ^b  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b University of Dayton   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMPUTATIONAL GEOMETRY; COMPUTER SIMULATION; LIFT; PRESSURE; SENSITIVITY ANALYSIS; SHEAR FLOW; SURFACE MEASUREMENT;

AERODYNAMIC LIFT; FOURTH ORDER EQUATION; SHEAR CENTER; TRAILING EDGE CONTROL SURFACE; VARIABLE GEOMETRY;

AIRFOILS;

EID: 0042510685     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (7)

1. Pendleton, E., Bessette, P., Field, P., Miller, G., and Griffin, K., "Active Aeroelastic Wing Flight Research Program: Technical Program and Model Analytical Development," Journal of Aircraft, Vol. 37, No. 4, 2000, pp. 554-561.
2. Kudva,J. N., Sanders, B., Pinkerton-Florance, J., Garcia, E., "Overview of the DARPA/AFRL/NASA Smart Wing Phase 2 Program," Proceedings of the 8th Annual International Symposium on Smart Structures and Materials, Industrial and Commercial Applications of Smart Structures Technologies, Mar. 4-6, 2001, pp. 390-398.
3. Sanders, B., Martin, C., Cowen, D., "Aerodynamic and Aeroelastic Characteristics of the DARPA Smart Wing Phase II Wind Tunnel Model," Proceedings of the 8th Annual International Symposium on Smart Structures and Materials, Industrial and Commercial Applications of Smart Structures Technologies, Mar. 4-6, 2001, pp. 383-389.
4. Sanders, B., Eastep, F.E., Forster, E., "Aerodynamic and Aeroelastic Characteristics of Wings with Conformal Control Surfaces for Morphing Aircraft," Journal of Aircraft, Vol. 40, No. 1, 2003, pp. 94-99.
5. Katz, J. and Plotkin, A., Low-Speed Aerodynamics, From Wing Theory to Panel Methods, McGraw-Hill, New York, 1991, pp. 125-134.
6. Prock, B., Weisshaar, T., Crossley, W., "Morphing Airfoil Shape Change Optimization with Minimum Actuator Energy as an Objective," AIAA 2002-5401, 9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, 4-5, Sept., 2002, Atlanta, GA.
7. Forster, E., Sanders, B., Eastep, F., "Synthesis of a Variable Geometry Trailing Edge Control Surface," AIAA-2003-1717, 44th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference, 7-10 April, 2003, Norfolk, VA.