YASim: Difference between revisions

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11 bytes added ,  23 December 2017
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note template does not like "=" in text
(Update for version 2018.1)
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{{Warning| Using YASIM_VERSION_CURRENT might make the aircraft unusable in case of future changes to YASim without updating the aircraft accordingly.}}
{{Warning| Using YASIM_VERSION_CURRENT might make the aircraft unusable in case of future changes to YASim without updating the aircraft accordingly.}}


New in 2018.1
'''New in 2018.1'''
*  '''mtow-lbs''' and '''mtow-kg:''' use (exactly) one of them to specify max. takeoff weight
*  '''mtow-lbs''' and '''mtow-kg:''' use (exactly) one of them to specify max. takeoff weight


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=== Wing Section Support ===
=== Wing Section Support ===
Many airliners have wings with a geometry that is just a little more complex than what YASim supported initially (tapered wing with some angles like sweep, dihedral, ...), e.g. they have an inboard section and an outboard section that can be described with YASim wing syntax. You can use a wing + a mstab XML element to describe this geometry but it is easier if YASim can just append more wing sections by simply adding more wing XML elements. This is now (Version 2018.1) possible, yasim will simply append sections if it finds more than one wing or hstab in the XML.
Many airliners have wings with a geometry that is just a little more complex than what YASim supported initially (tapered wing with some angles like sweep, dihedral, ...), e.g. they have an inboard section and an outboard section that can be described with YASim wing syntax. You can use a wing + a mstab XML element to describe this geometry but it is easier if YASim can just append more wing sections by simply adding more wing XML elements. This is now (Version 2018.1) possible, yasim will simply append sections if it finds more than one wing or hstab in the XML.
You should use <wing append="1" ... > for all but the first wing/hstab declaration.  
You should use '''<wing append="1" ... >''' for all but the first wing/hstab declaration.  
{{Note| YASim will ignore the root point x,y,z, the chord length and the incidence attributes, if you add append="1" and calculate those from the previous wing section. }}
{{Note|YASim will ignore the root point (x,y,z), the chord length and the incidence attributes, if you add "append" and calculate those from the previous wing section. }}
MAC calculation works for the whole wing.
MAC calculation works for the whole wing.


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