Publication | Closed Access
New solution method for steady-state canopy structural loads
19
Citations
3
References
1988
Year
New Computer CodeEngineeringStructural ApplicationComputer-aided DesignStructural OptimizationComputational MechanicsStructural SystemStructural EngineeringSuspension StructureNew Solution MethodAircraft Design ProcessGeometric ModelingDesignStructural DesignAerostructureAerospace EngineeringCivil EngineeringStructural AnalysisAeroelasticityAerodynamicsStructural MechanicsNew Code
A new computer code has been written to perform structural analysis of canopies. Although an existing code, CANO, has been available, the new code has better convergence reliability, is more understandably written, and is easier to use. The equations have been reformulated for the new solution method. The new code assumes a symmetric canopy, a steady-state condition, and no strength in the vertical direction. It computes the inflated shape, loads in the horizontal members, radial members, vent lines, suspension lines, and total drag. Constructed geometry, material properties, dynamic pressure, and pressure distribution are required as input.
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