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Wingflexer: Difference between revisions
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→How to add to your aircraft: fix m_fuel
(nasal implementation, link) |
m (→How to add to your aircraft: fix m_fuel) |
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</params> | </params> | ||
</PropertyList> | </PropertyList> | ||
Also adjust the property node aliases for the wing fuel tanks. Wingflexer supports up to four tanks in total. Since we're currently only solving one equation and hence get only one deflection which is used for both wings, we have to average the wing mass. | Also adjust the property node aliases for the wing fuel tanks. Wingflexer supports up to four tanks in total. Since we're currently only solving one equation and hence get only one deflection which is used for both wings, we have to average the wing mass. Internally, m_fuel is simply the sum of all given fuel nodes, | ||
m_fuel = | m_fuel = fuel-node-1-kg + fuel-node-2-kg + fuel-node-3-kg + fuel-node-4-kg | ||
so you must include the weighting factor in fuel-frac (e.g. 1/2 if you provide 2 fuel nodes). If you have more than 4 wing tanks in total, use another property rule to compute the average. | |||
In $yourAircraft-set.xml, in <systems> section, load the parameters and the wingflexer module: | In $yourAircraft-set.xml, in <systems> section, load the parameters and the wingflexer module: | ||