C₀ =
C₁ =
←α,C,T
T₀ =
T₁ =
←α,C,T
☺
α =
\(\alpha=\dfrac{\dfrac{C_1}{C_0}-1}{T_1-T_0}\)
⌂ Index
☺
Verzió: 2025-03-25 (
2012-03-19
..
2025-03-10 18:00:01
UTC )
gg630504