Fidelity Geometry module to model full aircraft with
regimes that cover all Mach numbers including
Mach AIC matrices as archival data entities for repetitive
point flutter solutions using K / P-K / g methods with true
Flutter Mode Tracking procedure with structural parametric
Spline module provides accurate FEM/Aero displacements and
Data Importer to process all NASTRAN/FEM modal output.
Memory and Database Management Systems establish subprogram
architecture allows user direct access to data entities
Data Input minimizes user learning curve while relieving
user input burden
display of aerodynamic models, Cp's, flutter
modes/ curves with PATRAN/TECPLOT/EXCEL, etc.
control allows massive flutter/ASE/Gust inputs and solution