ZAero Analysis

Structure for the Analysis tuple = ("Case Name", "Value"). "Case Name" defines the reference name for the subcase being specified. The "Value" must be a JSON String dictionary.

Analysis JSON String Dictionary

For the JSON string "Value" dictionary (e.g. "Value" = {"discipline": "LinearFlutter", "uaic": "cruise"}) the following keywords ( = default values) may be used:

• discipline = ""
  Analysis discipline JSON string. Options :
  LinearFlutter or flutter - Linear flutter
  ParamFlutter or fltpram - Parametric flutter.
  Aeroservoelastic or ase - Asymmetric parametric flutter.
  StaticAeroelastic or trim - Static areoelastic (see StaticAeroelastic or Trim Discipline JSON String Dictionary).
  EjectionLoads or eloads - Transient ejection loads.
  ManeuverLoads or mloads - Transient manouver loads.
  GustLoads or gloads - Discrete gust load.
  MFTGustLoads or mftgust - Continuous gust load.
  NonLinearFlutter or nlfltr - Nonlinear flutter.
  

• uaic = ""
  Name of the UAIC module for the subcase

StaticAeroelastic or Trim Discipline JSON String Dictionary

For the JSON string "Value" dictionary (e.g. "Value" = {"dynamicPressure": rho*V^2/2, "gravityAcceleration": 9.81 m/s^2}) the following keywords ( = default values) may be used:

• dynamicPressure
  Dynamic pressure

• vectorToCG = [0,0,0]
  Vector to offset the CG

• gravityAcceleration = NULL
  Gravity acceleration

• weight = NULL
  Weight of the overall aircraft if specified

• weightMomentOfInertia = NULL
  Moments of inertia of the full aircraft if specified: [IXX, IXY, IYY, IXZ, IYZ, IZZ]