strip Element |
Aerodynamic force- and moment coefficients of a fuselage strip
Namespace: Empty
Schema: Empty
Name | Occurrences | Description |
---|---|---|
Sequence | ||
cfx | [0, 1] | Force coefficient in CPACS-x direction |
cfy | [0, 1] | Force coefficient in CPACS-y direction |
cfz | [0, 1] | Force coefficient in CPACS-z direction |
cmx | [0, 1] | Moment coefficient in CPACS-x direction |
cmy | [0, 1] | Moment coefficient in CPACS-y direction |
cmz | [0, 1] | Moment coefficient in CPACS-z direction |
reference | Reference values for local aerodynamic coefficients. |
Name | Type | Required | Description |
---|---|---|---|
externalDataDirectory | string | ||
externalDataNodePath | string | ||
externalFileName | string |
This type can contain a complete set of aerodynamic force- and moment coefficients for a fuselage strip. It also includes the local reference values belonging to the strip coefficients. All coefficients act in the CPACS coordinate system. See the documentation for the global CPACS-Element for further information.
Force coefficient in (global, i.e. CPACS) x-direction, normalized with the local reference area.
Force coefficient in (global, i.e. CPACS) y-direction, normalized with the local reference area.
Force coefficient in (global, i.e. CPACS) z-direction, normalized with the local reference area.
Moment coefficient around the (global, i.e. CPACS) x-axis and the local reference point, normalized with the local reference area and reference length.
Moment coefficient around the (global, i.e. CPACS) y-axis and the local reference point, normalized with the local reference area and reference length.
Moment coefficient around the (global, i.e. CPACS) z-axis and the local reference point, normalized with the local reference area and reference length.
Reference values for the strip's coefficients. Moment reference point is given in absolut CPACS coordinates, i.e. x,y,z.