Static aeroelastic response of chiral-core airfoils

Journal of Intelligent Material Systems and Structures

Volumn 18, Issue 10, 2007, Pages 1067-1075

  Spadoni, A ^a   Ruzzene, M ^a  

^a Georgia Institute of Technology   (United States)

Author keywords

Chiral geometry; Passive morphing; Truss core airfoil

Indexed keywords

AERODYNAMICS; COMPUTATIONAL FLUID DYNAMICS; STRUCTURAL ANALYSIS; TWO DIMENSIONAL;

CHIRAL GEOMETRY; PASSIVE MORPHING; TRUSS-CORE AIRFOIL;

AIRFOILS;

EID: 34548706598     PISSN: 1045389X     EISSN: 15308138     Source Type: Journal    
DOI: 10.1177/1045389X06072361     Document Type: Article

References (14)

1. Bae, J.S., Seigler, T.M., Inman, D.J. and Lee, I. 2004. '' Aerodynamic and Aeroelastic Consideration of a Variablespan Morphing Wing, '' In: AIAA-2004-1726, 45th AIAA/ASME/ASCE/AHS/ ASC Structures, Structural Dynamics and Materials Conference, Palm Springs, California, April 19-22.
2. Bornengo, D., Scarpa, F. and Remillat, C. June 2005. '' Morphing Airfoil Concept with Chiral Core Structure, '' In: Proceedings of the I MECH E Part G, Journal of Aerospace Engineering, G3 (8). 185 - 192.
3. Bowman, J., Sanders, B. and Weisshaar, T. 2002. '' Identification of Military Morphing Aircraft Missions and Morphing Technology Assessment, '' In: Proceedings of SPIE Smart Materials and Structures, 17 March, San Diego, CA, pp. 121-132.
4. Buter, A., Ehlert, U.C., Sachau, D. and Breitbach, E. 2000. '' Adaptive Rotor Blade Concepts, Direct Twist and Camber Variation, '' In: AVT Symposium, Braunschweig.
5. Cadogan, D., Smith, T., Uhelsky, F. and Mac Cusick, M. 2004. '' Morphing Airfoil Wing Development for Compact Package Unmanned Aerial Vehicles, '' In: AIAA-2004-1807, 45th AIAA/ ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Palm Springs, CA, 19-22 April.
6. Campanile, L.F. and Sachau, D. 2000. '' The Belt-Rib Concept: A Structronic Approach to Variable Camber, '' Journal of Intelligent Materials Systems and Structures, 11(3): 215-224.
7. Cook, R.D., Malkus, D.S., Plesha, M.E. and Witt, R.J. 2001. Concepts and Applications of Finite Element Analysis, 4 th edn, Vol. II, Wiley, New York, NY.
8. Kudva, J.N. 2004. '' Overview of the DARPA Smart Wing Project, '' Journal of Intelligent Materials Systems and Structures, 15 (4). 261 - 267.
9. McGowan, A.R., Cox, D.E., Lazos, B.S., Waszak, M.R., Raney, D.L., Siochi, E.J. and Pao, P.S. 2003. '' Biologically Inspired Technologies in NASA's Morphing Project, '' In: Proceedings of SPIE Smart Structures and Materials, 15-20 March, San Diego, CA, pp. 1-13.
10. Mohammadi, B. 1994. '' Fluid Dynamics Computation with NSC2KE, '' INRIA Report 0164.
11. Monner, H.P., Sachau, D. and Breitbach, E. 1999. '' Design Aspects of the Elastic Trailing Edge for an Adaptive Wing, '' pp. 14 / 1 - 14 / 8, Research and Technology Agency, Ottawa, Canada, 18-21 October.
12. Prall, D. and Lakes, R.S. 1996. '' Properties of a Chiral Honeycomb with Poisson's ratio of -1, '' International Journal of Mechanical Sciences, 39 (3). 305 - 314.
13. Spadoni, A., Ruzzene, M. and Scarpa, F. 2005. '' Dynamic Response of Chiral Truss-Core Assemblies, '' Journal of Intelligent Materials Systems and Structures, 17 (11). 941 - 952.
14. Trenker, M. 2003. '' Design of Adaptive Airfoils with Dynamic Transonic Flow Control, '' Journal of Aircraft, 40 (4). 734 - 740.