Nonlinear aeroelastic analysis of joined-wing aircraft with fully intrinsic equations

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

Volumn , Issue , 2009, Pages

  Sotoudeh, Zahra ^a   Hodges, Dewey H ^a  

^a Georgia Institute of Technology   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTICITY; AIRCRAFT; AVIATION; CONTROL NONLINEARITIES; DESIGN AIDS; NONLINEAR EQUATIONS; STRUCTURAL DYNAMICS;

FINITE ROTATIONS; INTRINSIC EQUATION; JOINED WING CONFIGURATION; JOINED-WING AIRCRAFT; KINE-MATICAL EQUATIONS; MULTIPLE LOADS; NONLINEAR AEROELASTIC ANALYSIS; STATICALLY INDETERMINATE STRUCTURE;

WINGS;

EID: 84855623823     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2009-2464     Document Type: Conference Paper

References (9)

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2. Patil, M. J., "Nonlinear Aeroelastic Analysis of Joined-Wing Aircraft," Proceedings of the 44th Structures, Structural Dynamics and Materials Conference, Norfolk, Virginia, AIAA, Reston, Virginia, April 7 - 10, 2003.
3. Dreibelbis, B. and Barth, J., "Structural Analysis of Joint Wings," Proceedings of Regional Student Conference, AIAA, Baltimore, Maryland, April 2003.
4. Cesnik, C. E. S. and Su, W., "Nonlinear Aeroelastic Modeling and Analysis of Fully Flexible Aircraft," Proceedings of 46th Structures, Structural Dynamics and Materials Conference, Austin, Texas, AIAA, Reston, Virginia, April 18 - 21, 2005.
5. Cesnik, C. and Brown, E., "Active Warping Control of a Joined-Wing Airplane Configuration," Proceedings of 44th Structures, Structural Dynamics, and Materials Conference, Norfolk, Virginia, AIAA, Reston, Virginia, April 7 - 10, 2003.
6. Patil, M. J. and Hodges, D. H., "Flight Dynamics of Highly Flexible Flying Wings," Journal of Aircraft, Vol. 43, No. 6, 2006, pp. 1790-1799.
7. Hodges, D. H., "Geometrically-Exact, Intrinsic Theory for Dynamics of Curved and Twisted Anisotropic Beams," AIAA Journal, Vol. 41, No. 6, June 2003, pp. 1131 - 1137.
8. Peters, D. A., Karunamoorthy, S., and Cao, W.-M., "Finite State Induced Flow Models; Part I: Two-Dimensional Thin Airfoil," Journal of Aircraft, Vol. 32, No. 2, Mar.-Apr. 1995, pp. 313 - 322.
9. Sotoudeh, Z., Chang, C.-S., and Hodges, D. H., "Validation Studies for Nonlinear Aeroelastic Trim and Stability of HALE Aircraft," CEAS/AIAA/DGLR International Forum on Aeroelasticity and Structural Dynamics, Seattle, Washington, June 22 - 24, 2009, to appear.