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(→Command Line: added advanced usage notes) |
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Note that the above are for the aircraft taken as a whole, as solved by YASim, so they differ from the values of the wing airfoil. | Note that the above are for the aircraft taken as a whole, as solved by YASim, so they differ from the values of the wing airfoil. | ||
To get the tabular output for the example above at 1000 ft and 150 knots one would issue: | |||
<code>"C:\Program Files\FlightGear\bin\Win32\yasim.exe" "C:\Program Files\FlightGear\data\Aircraft\777-200\777-200ER.xml" -g -a 1000 -s 150</code> | |||
=== YASim design notes === | === YASim design notes === |
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