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301 bytes added, 09:48, 29 April 2019
+related links: Readme file and source code
Both the decrease of the pitot pressure and the default stall angle are based on a measurement
on an AN5812 pitot tube.
== Related content ==
=== Readme file ===
* {{readme file |systems}}
=== Source code ===
* {{flightgear source |path=src/Systems/pitot.hxx}}
* {{flightgear source |path=src/Systems/pitot.cxx}}
* {{flightgear source |path=src/Systems/static.hxx}}
* {{flightgear source |path=src/Systems/static.cxx}}
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