Kinematically designed flexible skins for morphing aircraft

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

Volumn , Issue , 2006, Pages

  Pastor, Christine ^a   Sanders, Brian ^b   Joo, James J ^c   McCarty, Robin ^a  

^a UNIVERSITY OF DAYTON   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

^c Dayton Research Institute   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT MANUFACTURE; DEFORMATION; FIBER REINFORCED MATERIALS; KINEMATICS; MACHINE DESIGN; SHAPE OPTIMIZATION;

CROSS LINK DENSITY; FLEXIBLE MATERIALS; RESISTIVE HEATING; SHAPE MEMORY POLYMER (SMP);

FLEXIBLE STRUCTURES;

EID: 85196550461     PISSN: 07334230     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/IMECE2006-13771     Document Type: Conference Paper

References (12)

1. TA Instruments ARES - RDA. 2005. TA Instruments. 24 May 2006 〈http://www.tainstruments.com/product.asp?n=1&id=32〉.
2. Veriflex(R). 2006. CRG Industries, LLC. 24 May 2006 〈http://www.crg-industries.com/veriflex.htm〉.
3. Bortolin, Robert Sebastian. "Characterization of Shape Memory Polymers for use as a Morphing Aircraft Skin Material." (2005).
4. DeCamp, Ronald W., Richard Hardy, Douglas K. Gould, "Mission- Adaptive Wing." SAE International Pacific Air and Space Technology Conference, Melbourne, Australia, 1987.
5. Dunne, J., D. Pitt, E. White, E. Garcia, 2000. "Ground Demonstration of the Smart Inlet." AIAA 41st Structures, Structural Dynamics, and Materials Conference, Atlanta, Georgia, April 2000
6. Hudson, Alvin & Rex Nelson,. University Physics. New York: Harcourt Brace Jovanovich, Inc., 1982.
7. Incropera, Frank P. and David P. DeWitt,. Fundamentals of Heat and Mass Transfer. : John Wiley & Sons, Inc., 2002.
8. Kudva, J.N. "Overview of the DARPA/AFRL/NASA Smart Wing Phase 2 Program." Journal of Intelligent Material Systems and Structures 15 (2004): 261-267.
9. Ozlslk, M. Necati. Heat Conduction: Second Edition. New York: John Wiley & Sons, Inc., 1993.
10. Perkins, David A., et al. "Morphing Wing Structures for Loitering Air Vehicles." 45th AIAA/ASME/ASCE/AHS/ASC Structures. Structural Dynamics & Materials Conference (2004).
11. Sepe, M.P. (1998). Dynamic Mechanical Analysis for Plastics Engineering. William Andrew Publishing/Plastics Design Library. Online version available at: http://www.knovel.com/knovel2/Toc.jsp?BookID=380&VerticalID=0
12. Toensmeier, P.A., "Morphing Aircraft Could Bring Multi-Role Capability to Next Generation Aircraft, Aviation Week,May 2005, pg 72-73