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Thermo 3 teil 2



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Mass flow (velocity triangle)

m˙ = ρ · A · C_x

Ideal pump work

Isentropic ideal gas equations T_2/T_1 to v

Isentr. turbine efficiency

Specific Enthalpy of Gases

h = u + pv

Isentropic Compression

h2 = h1 + v1 (p2 − p1)

Thermal efficiency

ηthermal =W_out/Q_in

Nassdampfgebiet mit x interpolieren:

h = h_f + x(h_g-h_f)

Ideal Gas equations

pv = RT

p = ρRT

Isentr. compressor efficiency

1st Law of Thermodynamics

W˙ − Q˙ = ˙m ( h1 − h2 + (v12−v22)/ρ + g (z1 − z2) )

Thermal coefficients

R = cp − cv

γ = k = cp/cv

Euler work

delta_h = U*delta C_theta

Linear interpolation

Isentropic ideal gas equations T_2/T_1 to p

Isentropic ideal gas equations p_2/p_1 to v

Nassdampfanteil X

X = (s-s_f)/)s_g-s_f)

Rotational speed

U = ω · r = 2π · f · r

const volume / pressure

h = c*T

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