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Maneuver trim optimization techniques for Active Aeroelastic Wings

Dimitri N. Mavris | Daniella E. Raveh | Paul Scott Zink

[1] M. Karpel,et al. Modal-Based Structural Optimization with Static Aeroelastic and Stress Constraints , 1997 .

[2] G. Vanderplaats,et al. Structural optimization by methods of feasible directions. , 1973 .

[3] M. Love,et al. An ASTROS application with path dependent results , 1996 .

[4] Raymond M. Kolonay,et al. Multiple control surface utilization in active aeroelastic wing technology , 1997 .

[5] Raymond M. Kolonay,et al. Optimization of a generic fighter wing incorporating active aeroelastic wing technology , 1996 .

[6] G. Dantzig,et al. Notes on Linear Programming: Part 1. The Generalized Simplex Method for Minimizing a Linear Form under Linear Inequality Restraints , 1954 .

[7] W. P. Rodden,et al. Equations of motion of a quasisteady flight vehicle utilizing restrained static aeroelastic characteristics , 1985 .

[8] Dimitri N. Mavris,et al. Robust Design for Aeroelastically Tailored/Active Aeroelastic Wing , 1998 .

[9] D. J. Neill,et al. ASTROS - A multidisciplinary automated structural design tool , 1987 .

[10] G. Miller. An active flexible wing multi-disciplinary design optimization method , 1994 .