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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.