 ZAERO in NE/NASTRANby Zona Technology ZAERO by ZONA Technologies Inc., has extensive capabilities in the  areas of aero-elasticity, aeroservoelasticity, unsteady aerodynamics and  structural dynamics. 
 
   
  
    
      
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       ZAERO
      in NE/NASTRAN 
       
       
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          ZAERO
          by ZONA Technologies Inc., has extensive capabilities in the 
          areas of aero-elasticity, aeroservoelasticity, unsteady aerodynamics
          and  structural dynamics. Since its incorporation in 1986, ZONA
          has been serving the aerospace structural dynamics community through
          contractual work and software licensing support.
         
       
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                    High
                    Fidelity Geometry module to model full aircraft with 
                    stores/nacelles.
                   
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                    Flight
                    regimes that cover all Mach numbers including
                    transonic/hypersonic ranges.
                   
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                    Unified
                    Mach AIC matrices as archival data entities for repetitive
                    structural design/analysis.
                   
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                    Matched/non-matched
                    point flutter solutions using K / P-K / g methods with true
                    damping.
                   
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                    Built-in
                    Flutter Mode Tracking procedure with structural parametric 
                    sensitivity analysis.
                   
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                    3D
                    Spline module provides accurate FEM/Aero displacements and
                    forces transferal.
                   
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                    Modal
                    Data Importer to process all NASTRAN/FEM modal output.
                   
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                    Dynamic
                    Memory and Database Management Systems establish subprogram 
                    modularity.
                   
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                    Open
                    architecture allows user direct access to data entities
                   
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                    Bulk
                    Data Input minimizes user learning curve while relieving
                    user input burden
                   
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                    Graphic
                    display of aerodynamic models, Cp's, flutter 
                    modes/ curves with PATRAN/TECPLOT/EXCEL, etc.
                   
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                    Executive
                    control allows massive flutter/ASE/Gust inputs and solution 
                    outputs.
                   
                 
               
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