俺のT-4こんな感じ [TurbineEngineData] fuel_flow_gain= 0.0025//0.01 inlet_area= 15.20 rated_N2_ rpm = 29950.00 static_thrust= 21950.00
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俺のT-4こんな感じ
[TurbineEngineData]
fuel_flow_gain= 0.0025//0.01
inlet_area= 15.20
rated_N2_rpm= 29950.00
static_thrust= 21950.00
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