New aeroelastic studies for a morphing wing

48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition

Volumn , Issue , 2010, Pages

  Courchesne, Samuel ^a   Popov, Andrei Vladimir ^a   Botez, Ruxandra Mihaela ^a  

^a LARCASE   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

A-CARBON; AEROELASTIC INSTABILITIES; AEROSPACE RESEARCH; ANGLES OF ATTACK; FINITE ASPECT RATIO; LIMIT SPEED; MORPHING; MORPHING WINGS; NATIONAL RESEARCH COUNCIL; NEW STUDY; SHAPE MEMORY ALLOY; TEST CASE; UPPER SURFACE; WIND TUNNEL TESTS;

AEROSPACE ENGINEERING; AIRFOILS; ANGLE OF ATTACK; ASPECT RATIO; FLEXIBLE WINGS; FLUTTER (AERODYNAMICS); MACH NUMBER; REYNOLDS NUMBER; WIND STRESS; WIND TUNNELS;

AEROELASTICITY;

EID: 78649809522     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)

1. th AIAA Aviation Technology, Integration and Operations Conference (ATIO), 18-20 September, pp. 1-9.
2. Bharti, S. et al., 2006, Optimal structural design of a morphing aircraft wing using parallel nondominated sorting genetic algorithm II (NSGA II), Smart Structures and Materials 2006: Industrial and commercial applications of smart structures technologies, edited by D. K. Lindner, Proceedings of SPIE Vol. 6166, pp. 1-12.
3. Sanders, B. et al., 2003, Aerodynamic and aeroelastic characteristics of wings with conformal control surfaces for morphing aircraft, Journal of Aircraft, Vol. 40(1), pp. 94-99.
4. Coutu, D., Brailovski, V., Terriault, P., 2009, Promising Benefits of an Active-Extrados Morphing Laminar Wing, Journal of Aircraft, Vol. 46(2), pp. 730-731.
5. MSC/Nastran documentation (MSC software corporation, USA), 2001.
6. FAR 25 Aviation Regulations, 2000.