Difference between revisions of "Template:VT"
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m (Use new mass template) |
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<includeonly>{{#expr: <!-- | <includeonly>{{#expr: <!-- | ||
--> ( <!-- | --> ( <!-- | ||
− | --> 2 * {{G}} * {{Body data|{{{planet|{{{1}}}}}} | + | --> 2 * {{G}} * {{Body data/Mass|{{{planet|{{{1}}}}}}}} <!-- |
--> / ( <!-- | --> / ( <!-- | ||
--> ({{{alt|{{{2}}}}}} + {{Body data|{{{planet|{{{1}}}}}}|radius}} <!-- | --> ({{{alt|{{{2}}}}}} + {{Body data|{{{planet|{{{1}}}}}}|radius}} <!-- | ||
--> )^2 * <!-- | --> )^2 * <!-- | ||
− | --> ( {{ | + | --> ( {{Body data|{{{planet|{{{1}}}}}}|pressure}} * e^(-{{{alt|{{{2}}}}}}/{{Body data|{{{planet|{{{1}}}}}}|scale height}}) <!-- |
--> ) * (1.2230948554874 * 0.008) * 0.2 * 1 <!-- | --> ) * (1.2230948554874 * 0.008) * 0.2 * 1 <!-- | ||
--> ) <!-- | --> ) <!-- | ||
--> ) ^ 0.5 {{#if: {{{3|{{{round|}}}}}}|round {{{3|{{{round}}}}}}}}}}</includeonly><noinclude> | --> ) ^ 0.5 {{#if: {{{3|{{{round|}}}}}}|round {{{3|{{{round}}}}}}}}}}</includeonly><noinclude> | ||
+ | {{Outdated| | ||
+ | * This is almost certainly outdated due to the atmospheric physics changes in [[1.0]]. | ||
+ | }} | ||
{| class="wikitable" | {| class="wikitable" | ||
! Usage || Produces | ! Usage || Produces | ||
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|} | |} | ||
− | This template calculates terminal velocity of an object given the planet and the altitude from the planet's surface. It uses {{Tl| | + | This template calculates terminal velocity of an object given the planet and the altitude from the planet's surface. It uses {{Tl|Body data}} with the properties <tt>mass</tt>, <tt>radius</tt>, <tt>pressure</tt> and <tt>scale height</tt>. |
{{Parameter table|name=both|parameters= | {{Parameter table|name=both|parameters= |
Latest revision as of 11:41, 12 May 2018
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|
Usage | Produces |
---|---|
{{VT | planet = Kerbin | alt = 0}} |
100.1288989294 |
This template calculates terminal velocity of an object given the planet and the altitude from the planet's surface. It uses {{Body data}} with the properties mass, radius, pressure and scale height.
#/Name | Optional | Description | Default |
---|---|---|---|
1 or planet | No | The celestial body | |
2 or alt | No | The altitude at which the terminal velocity should be calculated. | |
3 or round | Yes | Round to the given number of decimal places. | Not set/Doesn't round |
(M is the mass of the body, r is the body's radius, p0 is pressure at 0 m altitude (“sea level”), a is the altitude above sea level and H is the scale height)
The formula assumes that the coefficient of drag (d) is 0.2 and is used from the atmosphere article.