Aerodynamic and aeroelastic considerations of a variable-span morphing wing

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

Volumn 3, Issue , 2004, Pages 2378-2386

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

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

^b Korea Advanced Institute of Science and Technology (KAIST)   (South Korea)

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

^d Department of Aerospace Engineering ^*  (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; AIRFOILS; BENDING MOMENTS; DEFORMATION; DENSITY (SPECIFIC GRAVITY); DRAG; MISSILES; OPTIMIZATION; SPACE RESEARCH; UNMANNED VEHICLES; WINGS;

AIR DENSITY; UNMANNED AIR VEHICLES (UAV); VARIABLE-SPAN MORPHING WING (VSMW); WINGSPAN;

AERODYNAMICS;

EID: 16244421706     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-1726     Document Type: Conference Paper

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, July-August, 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, Mar., 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, Sep. 1991, pp. 572-578.
9. Bae, J. S., Seigler, T. M., and Inman, D. J., "Aerodynamic and Static Aeroelastic Characteristics of a Variable-Span Morphing Wing," Journal of Aircraft, 2004, accepted for publication.
10. Anderson, J. D., Jr., Introduction to Flight, McGraw-Hill, New York, 1985, pp. 298-303