Add info about weight and Cd and modify eda
This commit is contained in:
parent
1974be7faf
commit
30bbccb98d
1 changed files with 5 additions and 5 deletions
|
@ -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>
|
||||
|
|
Loading…
Reference in a new issue