flightloads.pdf

节选段落一：
Figure 1-2 FlightLoads Integration of MSC.Nastran and MSC.Patran
The MSC.Patran component of FlightLoads provides access to the user’s CAD system for basic
geometry information (STEP or IGES sources are also supported) and then creates the
aerodynamic and structural models that are used in calculating


节选段落二：
If the user chooses an Analysis Type of Structural or Thermal,
FlightLoads is subsequently accessed in an existing database through the Preferences/Analysis
menu. FlightLoads coexists with the available structural and thermal analyses in the
MSC.Nastran Preference as an aeroelastic analysis.


节选段落三：
File Group Viewport Display Preferences Tools Help
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MSC.FlightLoads
FlightLoads & Dynamics
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Aeroelasticity
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