dragContributionsType Complex Type |
Drag contributions
Namespace: Empty
Schema: Empty
Name | Occurrences | Description |
---|---|---|
All | ||
cdFriction | [0, 1] | Drag contributions due to friction |
cdInduced | [0, 1] | Drag contributions due to energy loss through vortex structures caused by the pressure difference between the upper and lower sides of three-dimensional lifting surfaces. |
cdInterference | [0, 1] | Drag contributions due to mixing of streamlines between airframe components (e.g., interaction between wing and fuselage or pylon and wing). |
cdPressure | [0, 1] | Drag contributions due to the displacement of the flow around a component. Zero for irrotational two-dimensional flows. |
cdTrim | [0, 1] | Drag contributions due to trimmed aircraft configuration |
cdViscous | [0, 1] | Drag contributions due to shear forces on surfaces |
cdWave | [0, 1] | Drag contributions due to energy dissipation in shock waves |
Name | Type | Required | Description |
---|---|---|---|
externalDataDirectory | string | ||
externalDataNodePath | string | ||
externalFileName | string |