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Сообщение от Ice_Eagle
So that's a 'universal' setting then. What about laminar flow? Because just because there are big radiators hanging from the wing, engine nacelle, etc., doesn't necessarily mean big drag numbers.
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For each plane I calculate my parameter.
I rely on the power of the engine, also look closely at the drawings - profile, wing narrowing, thickness and other parameters.
Setting up tx for each individual aircraft requires some calculations and several tests.
If there are polars of the original, then tx comes out of the first test.
The speed difference is 1-3 km.
Mig-3 flew with his TTX from the first time.
For other models it is necessary to correct different figures in fm.
This is to bring the behavior of the virtual plane closer to the original.
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This is my hobby in life.
Someone is fishing or climbing high mountains, and I like to set up virtual planes.