Missile DATCOM Analysis Interface Module (AIM)
Missile DATCOM Analysis Interface Module (AIM)
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Missile DATCOM FinSet

Structure for the constraint tuple = ("FinSet Name", "Value"). "Constraint Name" defines the reference name for the constraint being specified. The "Value" can either be a JSON String dictionary (see Section JSON String Dictionary) or a single string keyword (see Section keyStringFinSet).

JSON String Dictionary

If "Value" is JSON string dictionary (eg. "Value" = {"Translation": "free", "Rotation":"free"}) the following keywords ( = default values) may be used:

  • SecNACA = ""
    Airfoil section type for the FinSet.
    For NACA, the full NACA control card should be specifed (without the FinSet index), e.g.:
    SecTyp = "NACA-4-0012"
    for a NACA 4-series airfoil. See the Missile Datcom NACA Control Card documentation for more info.
  • phif = <from geometry by default>
    List of roll angle of each fin measured clockwise from top vertical center looking forward.
    This overrides values otherwise computed from the geometry.
    Note: If both phif and gam are specified they must be of the same length.
  • gam = <from geometry by default>
    List of roll angle of each fin measured clockwise from top vertical center looking forward This overrides values otherwise computed from the geometry.
    Note: If both phif and gam are specified they must be of the same length.
  • nvor = 1
    Number of vortices shed from each panel, up to a maximum of 20