Aerodynamic and static aeroelastic characteristics of a variable-span morphing wing

Journal of Aircraft

Volumn 42, Issue 2, 2005, Pages 528-534

  Bae, Jae Sung ^a,b,c   Seigler, T Michael ^a,b   Inman, Daniel J ^a,b  

^a VIRGINIA POLYTECHNIC INSTITUTE AND STATE UNIVERSITY   (United States)

^b Ctr Intelligent Mat Syst/Struct   (United States)

^c Korea Institute of Energy Research (KIER)   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AEROSPACE ENGINEERING; ASPECT RATIO; BENDING MOMENTS; DEFORMATION; DRAG; FLIGHT DYNAMICS; MODAL ANALYSIS; PRESSURE EFFECTS; STIFFNESS; STIFFNESS MATRIX;

AERODYNAMIC FORCES; DRAG COEFFICIENTS; DYNAMIC PRESSURE; LIFT COEFFICIENTS;

WINGS;

EID: 18144389846     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.4397     Document Type: Article

References (10)

1. Bowman, J., Sanders, B., and Weisshaar, T., "Evaluating the Impact of Morphing Technologies on Aircraft Performance," AIAA Paper 2002-1631, April 2002.
2. Gern, F. H., Inman, D. J., and Kapania, R. K., "Structural and Aeroelastic Modeling of General Planform Wings with Morphing Airfoils," AIAA Journal, Vol. 40, No. 4, 2002, pp. 628-637.
3. Sanders, B., Eastep, F. E., and Foster, 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.
4. Amprikidis, M., and Cooper, J. E., "Development of Smart Spars for Active Aeroelastic Structures," AIAA Paper 2003-1799, April 2003.
5. Blondeau, J., Richeson, J., and Pines, D. J., "Design, Development and Testing of a Morphing Aspect Ratio Wing Using an Inflatable Telescopic Spar," AIAA Paper 2003-1718, April 2003.
6. Bae, J. S., Yang, S. M., and Lee, I., "Linear and Nonlinear Aeroelastic Analysis of a Fighter-Type Wing with Control Surface," Journal of Aircraft, Vol. 39, No. 4, 2002, pp. 697-708.
7. Ueda, T., and Dowell, E. H., "A New Solution Method for Lifting Surfaces in Subsonic Flow," AIAA Journal, Vol. 20, No. 3, 1982, pp. 348-355.
8. Eversman, W., and Pitt, D. M., "Hybrid Doublet Lattice/Doublet Point Method for Lifting Surfaces in Subsonic Flow," Journal of Aircraft, Vol. 28, No. 9, 1991, pp. 572-578.
9. Striz, A. G., and Venkayya, V. B., "Influence of Structural and Aerodynamic Modeling on Flutter Analysis," Journal of Aircraft, Vol. 31, No. 5, 1994, pp. 1205-1211.
10. Anderson, J. D., Jr., Introduction to Flight, McGraw-Hill, New York, 1985, pp. 298-303.