diff --git a/Docs/README.submodels b/Docs/README.submodels index 984ade06c..999038540 100644 --- a/Docs/README.submodels +++ b/Docs/README.submodels @@ -33,11 +33,6 @@ aircraft'snose. Right is positive. <pitch-offset> Submodel's initial elevation, in degrees, relative to user aircraft's pitch. Up is positive. - <eda> Equivalent Drag Area in ft squared. The object is assumed - to have a mass of 0.03 slugs and a drag coefficient of - 0.295, and sea-level air density is assumed. Adjust the - EDA to give the model the ballistics you need. - The default value is 0.007. <life> Life span in seconds. Default is 900.0. <buoyancy> In ft/sec/sec. Works opposite acceleration of gravity. For example, if set to 32 the submodel will feel no @@ -45,6 +40,11 @@ Default is 0. <wind> Set to true if you want the submodel to react to the wind. Default is "false". + <cd> The Coeffient of Drag. Varies with sabmodel shape - 0.295 for a bullet, + 0.045 for an airfoil. Enter an appropriate value. Defaults to 0.295. + <eda> Effective drag area (sq ft). Usually the cross-sectional area of the + submodel normal to the airflow. + <weight> The weight of the submodel (lbs). Defaults to 0.25 --> <PropertyList>