1001Ferramentas
♻️ Calculators

Regenerator Effectiveness

Calculate the effectiveness of a regenerator (heat recuperator), ε = (T_out − T_in) ÷ (T_hot − T_in), comparing the actual heating of the cold fluid with the maximum possible (if it reached the hot exhaust gas temperature). The result (between 0 and 1, or ×100%) measures heat-exchange effectiveness: a regenerator uses a gas turbine's exhaust heat to preheat the air before the combustor, cutting fuel use and raising the regenerative Brayton cycle efficiency. Typical effectiveness is 0.7–0.9. Enter the inlet, outlet and hot-gas temperatures.

Result

Regenerator effectiveness

In a gas turbine the exhaust gases leave very hot — while the compressed air enters the combustion chamber relatively cold. The regenerator (or recuperator) is a heat exchanger that exploits this gap: it uses the heat of the exhaust gas to preheat the air before combustion, so that less fuel is needed to reach the firing temperature — which raises the efficiency of the regenerative Brayton cycle. The effectiveness measures how well the regenerator does that job: ε = (T_out − T_in) ÷ (T_hot − T_in). The numerator is the actual heating of the air (how much it really warmed up); the denominator is the maximum possible heating, which would occur if the air came out as hot as the exhaust gas entering the regenerator. The ratio lies between 0 and 1: ε = 1 would mean an ideal exchanger (air preheated all the way to the gas temperature), impossible in practice. Real regenerators reach 0.7 to 0.9; higher values demand huge exchangers, with more pressure drop and more cost. Regeneration only pays off when the compressor pressure ratio is moderate, otherwise the compressed air already leaves the compressor too hot. Enter the inlet, outlet and hot-gas temperatures.

Related Tools

🔁

Back Work Ratio (BWR)

Calculate the back work ratio (BWR) of a power cycle, BWR = w_compressor ÷ w_turbine, dividing the work consumed by the compressor (or pump) by the gross work produced by the turbine. The dimensionless result shows what fraction of turbine work is reinvested to compress the fluid. In gas turbines (Brayton cycle) the BWR is high (0.4–0.6), since compressing gas is costly; in steam Rankine cycles it is tiny (~0.01), since pumping liquid is cheap. A high BWR makes the cycle sensitive to component efficiencies. Enter the compressor work and the turbine work.

Combined Cycle Efficiency

Calculate the efficiency of a gas-steam combined cycle, η_cc = η_gas + η_steam − (η_gas × η_steam ÷ 100), combining the gas turbine efficiency (Brayton, topping) with the steam cycle (Rankine, bottoming) that recovers heat from the exhaust gases. The result, in %, exceeds either cycle alone because the heat rejected by the gas turbine, instead of being wasted, raises steam for a second turbine. This is why modern combined-cycle plants top 60% efficiency, the highest in thermal generation. Enter the gas-cycle and steam-cycle efficiencies (in %).

🌡️

Welding Preheat Temperature

Estimate the preheat temperature for welding, Tp = 350·√(CE − 0.25), as a function of the steel's carbon equivalent (CE). Preheating reduces the cooling rate, giving hydrogen time to escape and preventing the formation of brittle martensite and cold cracks in the heat-affected zone. Steels with a high CE require more preheating. Enter the steel's carbon equivalent.

🌬️

Molar Mass from Gas Density

Enter density in g/L, temperature in K and pressure in atm: M = ρ·R·T/P with R = 0.08206. A gas at 1.96 g/L, 273 K and 1 atm gives 43.9 g/mol.

🌡️

Elenbaas Number

Computes the Elenbaas number of a channel formed by two heated vertical parallel plates, El = g·β·ΔT·b⁴ ÷ (ν·α·H), which is the Rayleigh number based on the plate spacing b multiplied by the ratio b/H. It governs natural convection in finned heat sinks, electronics enclosures and solar collectors: a very small El means a narrow, tall channel where the boundary layers merge and choke the flow, while a large El means the plates behave as isolated. The spacing that maximises a heat sink's total dissipation falls near El ≈ 46 for isothermal plates, a classic natural-convection fin design criterion. Gravity is taken as 9.80665 m/s², β is the fluid thermal expansion coefficient and H the plate height. Enter the expansion coefficient, the temperature difference, the spacing, the kinematic viscosity, the thermal diffusivity and the plate height.

🗑️

Landfill Methane Flow (Scholl Canyon)

Computes the methane flow generated by one batch of landfilled waste using the Scholl Canyon first-order decay model, Q = k × L₀ × M × e^(−k×t), where M is the mass of that batch, L₀ is the total methane potential per tonne, k is the annual decay constant and t is the age of the batch. The model assumes generation peaks right after placement and falls exponentially from then on, with k between 0.04 and 0.09 per year in wet climates and L₀ typically 50 to 170 m³ of methane per tonne of wet waste, 170 being the LandGEM default. Since the model is linear in mass, a real landfill is summed batch by batch, each with its own age. Enter the decay constant, the methane potential, the waste mass and the age of the batch.

The results provided by this tool are for general informational and educational purposes only and do not constitute professional, financial, medical, legal, tax or accounting advice. Always confirm important decisions with a qualified professional and official sources.