AIAA Journal · 1980 · 35 citations · 7 references
EngineeringCivil EngineeringDesignAircraft StructuresDesign OptimizationStructural EngineeringDamage ToleranceStructural DesignStructural IntegrityStructural MechanicsStructural OptimizationStructural ReliabilityAircraft Structural DesignDamage-tolerant DesignOptimal DesignOptimal Design Of TrussesOptimization Of Truss StructuresSensitivity Analysis For Tolerance DesignTruss Structure DesignTruss Systems
The basic idea presented herein is that a systematic method for optimal structural design can be developed that accounts for probable future damage to the structure. A general mathematical model for the damage-tolerant structure design problem is defined. Design sensitivity analysis and procedures for treatment of a large number of constraints for the problem are presented. As a practical design example, damage-tolerant design of an open truss helicopter tail-boom structure is considered. Optimal designs for several cases of the tail-boom are presented. It is shown that considerable design variation is necessary to achieve the damage-tolerant design objective. It is also shown that if the structure is optimized without consideration of damage, the structure will fail catastrophically when any damage occurs to the structure.
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Methods of Design Sensitivity Analysis in Structural Optimization
Jasbir S. Arora, Edward J. Haug · AIAA Journal · 1979 · 307 citations
FAIL-SAFE OPTIMAL DESIGN OF STRUCTURES
Peiqing Sun, Jasbir S. Arora, Edward J. Haug · Engineering Optimization · 1976 · 47 citations