Fluid statics and dynamics, pipe flow, boundary layers, aerodynamics, heat conduction, convection and radiation, heat exchangers, thermodynamic cycles, psychrometrics and combustion.
Thermofluids (thermofluids-ai999x) is an offline Python package for thermofluids. It covers fluid statics and dynamics, pipe flow, boundary layers, aerodynamics, heat conduction, convection and radiation, heat exchangers, thermodynamic cycles, psychrometrics and combustion.
It has 99 capabilities — 13 computational procedures and 86 formulas — in 20 topics, the largest being Pipe flow, Convection, Conduction, Gas processes, Heat exchangers and Psychrometrics. Ask a question in words with ask(), or call a capability by name with typed inputs with solve(). Every answer carries its value and unit, the steps that produced it and the formula in LaTeX.
When a question is not determined — a value is missing, an input is out of range, or the request is outside the package — it says so and names what it needs, instead of guessing. It runs on an ordinary CPU without a network connection (Python >=3.10), and the same question always gets the same answer.
pip install thermofluids-ai999x hf download AI999X/thermofluids-ai999x --local-dir thermofluids-ai999x
Each question below was put to thermofluids-ai999x and the answer shown is the one it returned, with the steps it took.
Water with density 998 kg/m^3 and dynamic viscosity 0.001 Pa*s flows at an average velocity of 1.5 m/s in a pipe of diameter 0.05 m. What is the Reynolds number?
rho = 998 kg/m^3, v = 1.5 m/s, D = 0.05 m, mu = 0.001 Pa*sRe = 74850 1Oil of density 900 kg/m^3 and viscosity 0.1 Pa*s flows in laminar flow at a mean velocity of 0.5 m/s in a pipe of diameter 0.02 m. What is the friction factor?
rho = 900 kg/m^3, v = 0.5 m/s, D = 0.02 m, mu = 0.1 Pa*sRe = 90 1Re = 90 1f = 0.7111111111 1An air-standard Otto cycle has a compression ratio of 8. What is its thermal efficiency?
r = 8 1eta = 0.5647247184 1Dew point temperature: T = 25 °C, RH = 60%
T = 25 °C, RH = 0.6T_dew = 289.8511319 K, p_v = 1901.529882 Pam.solve("lmtd", Th_in="150 °C", Th_out="90 °C", Tc_in="30 °C", Tc_out="70 °C", arrangement="counterflow") Th_in = 150 °C, Th_out = 90 °C, Tc_in = 30 °C, Tc_out = 70 °C, arrangement = counterflowlmtd = 69.52118994 K, dT1 = 80 K, dT2 = 60 KUsing thin airfoil theory, what is the lift coefficient of a symmetric airfoil at an angle of attack of 5 deg?
alpha = 0.0872664626 radCL = 0.5483113556 1Air flows over a flat plate with a laminar boundary layer and a Reynolds number of 250000 at the trailing edge. What is the average skin friction coefficient?
ReL = 250000 1cfm = 0.00265645869 1Methane with a lower heating value of 50000000 J/kg burns at an air-fuel ratio of 17.2 with a reactant temperature of 298 K. Taking the specific heat of the products as 1200 J/(kg*K), what is the adiabatic flame temperature?
T0 = 298 K, LHV = 50000000 J/kg, AFR = 17.2 1, cp = 1200 J/(kg*K)Tad = 2587.377289 KEvery snippet was run as shown; the output under it is what it printed.
import thermofluids_ai999x as m
a = m.ask("Water with density 998 kg/m^3 and dynamic viscosity 0.001 Pa*s flows at an average velocity of 1.5 m/s in a pipe of diameter 0.05 m. What is the Reynolds number?")
print(a.outcome)
print(a.value, a.unit)
for step in a.steps:
print(step["name"])SOLVED 74850.0 1 Reynolds number from density, velocity, diameter and viscosity
import thermofluids_ai999x as m
a = m.solve("lmtd", Th_in="150 °C", Th_out="90 °C", Tc_in="30 °C", Tc_out="70 °C", arrangement="counterflow")
print(a.outcome)
print(a.values)SOLVED
{'lmtd': 69.52118993564416, 'dT1': 80.0, 'dT2': 60.0}
import thermofluids_ai999x as m
# an input is missing: the answer says what it needs instead of guessing
a = m.solve("lmtd")
print(a.outcome)
print(a.message)NEEDS_INPUT
lmtd needs Th_in, Th_out, Tc_in, Tc_out, arrangement (hot stream inlet temperature; hot stream outlet temperature; cold stream inlet temperature; cold stream outlet temperature; flow arrangement). Example: solve('lmtd', Th_in='423.15 K', Th_out='363.15 K', Tc_in='303.15 K', Tc_out='343.15 K', arrangement='counterflow').
thermofluids-ai999x "Water with density 998 kg/m^3 and dynamic viscosity 0.001 Pa*s flows at an average velocity of 1.5 m/s in a pipe of diameter 0.05 m. What is the Reynolds number?"
Reynolds number = 74850 1 1. Reynolds number from density, velocity, diameter and viscosity: Re = rho*v*D/mu with rho = 998 kg/m^3, v = 1.5 m/s, D = 0.05 m, mu = 0.001 Pa*s -> Re = 74850 1 Assumptions: Newtonian fluid; the diameter as the characteristic length …
Every value in these figures was computed by the package, each point a run of solve(); in a notebook, plot() and plot_relation() draw a capability's curves the same way.
12 of its 99 formulas; every one is in the capability browser below.
Search by name, formula, input or topic. Each capability opens to show what it takes, what it returns, when it applies, and a question it answered.
thin_airfoil_lift_coefficientalpha angle of attack [rad]CL section lift coefficientblasius_average_skin_frictionReL Reynolds number based on the plate lengthcfm average skin-friction coefficient over the plateblasius_displacement_thicknessx distance from the leading edge [m]Rex local Reynolds number U x / nuds displacement thickness [m]blasius_local_skin_frictionRex local Reynolds number U x / nucf local skin-friction coefficientblasius_momentum_thicknessx distance from the leading edge [m]Rex local Reynolds number U x / nuth momentum thickness [m]adiabatic_flame_temperature_simpleT0 temperature of the reactants [K]LHV lower heating value of the fuel [J/kg]AFR air-fuel ratio by masscp mean specific heat of the products [J/(kg*K)]Tad adiabatic flame temperature [K]equivalence_ratioEquivalence ratio and excess air of a gaseous fuel burned at a given air-fuel ratio by mass.
fuel the fuel choiceafr actual air-fuel ratio by massphi equivalence ratio (fuel-air ratio over stoichiometric)afr_stoich stoichiometric air-fuel ratioexcess_air excess air as a fractionstoichiometric_air_fuel_ratioMass of air per mass of fuel for complete combustion, with the moles of O2 and air per mole of fuel.
fuel the fuel choiceafr_stoich stoichiometric air-fuel ratio (mass)o2_moles moles of O2 per mole of fuelair_moles moles of air per mole of fuelstagnation_pressure_airP static pressure [Pa]M Mach numberP0 stagnation pressure [Pa]mach_numberv mean flow velocity [m/s]a local speed of sound [m/s]M Mach numbernormal_shock_mach_airM1 Mach number ahead of the shockM2 Mach number behind the shockspeed_of_sound_ideal_gasgamma ratio of specific heatsR specific gas constant [J/(kg*K)]T absolute temperature of the gas [K]a speed of sound [m/s]stagnation_temperature_machT static temperature [K]gamma ratio of specific heatsM Mach numberT0 stagnation (total) temperature [K]normal_shock_pressure_airP1 static pressure ahead of the shock [Pa]M1 Mach number ahead of the shockP2 static pressure behind the shock [Pa]critical_insulation_radiusk thermal conductivity [W/(m*K)]h outside heat transfer coefficient [W/(m^2*K)]r critical outer radius of the insulation [m]plane_wall_conductionk thermal conductivity [W/(m*K)]A wall area [m^2]T1 inner surface temperature [K]T2 outer surface temperature [K]L wall thickness [m]q rate of heat transfer [W]overall_heat_rateU overall heat transfer coefficient [W/(m^2*K)]A wall area [m^2]Ti inside fluid temperature [K]To outside fluid temperature [K]q rate of heat transfer [W]wall_generation_max_temperatureTs surface temperature [K]q heat generated per unit volume [W/m^3]L half-thickness of the wall [m]k thermal conductivity [W/(m*K)]Tmax temperature at the mid-plane [K]overall_u_plane_wallh1 inside heat transfer coefficient [W/(m^2*K)]L wall thickness [m]k thermal conductivity [W/(m*K)]h2 outside heat transfer coefficient [W/(m^2*K)]U overall heat transfer coefficient [W/(m^2*K)]cylinder_conductionk thermal conductivity [W/(m*K)]L length of the cylinder [m]T1 inner surface temperature [K]T2 outer surface temperature [K]r1 inner radius [m]r2 outer radius [m]q rate of heat transfer [W]sphere_conductionk thermal conductivity [W/(m*K)]T1 inner surface temperature [K]T2 outer surface temperature [K]r1 inner radius [m]r2 outer radius [m]q rate of heat transfer [W]thermal_diffusivityk thermal conductivity [W/(m*K)]rho density of the material [kg/m^3]cp specific heat capacity [J/(kg*K)]alpha thermal diffusivity [m^2/s]flat_plate_laminar_average_nusseltReL Reynolds number based on the plate lengthPr Prandtl number of the fluidNu average Nusselt number over the platechurchill_bernstein_cylinderAverage Nusselt number of a circular cylinder in cross flow over the whole Reynolds range.
Re Reynolds number based on the diameterPr Prandtl numberNu average Nusselt number based on the diameterchurchill_chu_vertical_plateAverage Nusselt number of free convection from an isothermal vertical plate, laminar and turbulent.
Ra Rayleigh number based on the plate heightPr Prandtl numberNu average Nusselt numberdittus_boelter_coolingRe Reynolds numberPr Prandtl number of the fluidNu Nusselt numberdittus_boelter_heatingRe Reynolds numberPr Prandtl number of the fluidNu Nusselt numbergnielinski_nusseltNusselt number of fully developed turbulent or transitional flow in a tube.
Re Reynolds number (3000 to 5e6)Pr Prandtl number (0.5 to 2000)f Darcy friction factorNu Nusselt number based on the diameternusselt_heat_transfer_coefficientNu average Nusselt numberk thermal conductivity [W/(m*K)]Lc characteristic length (diameter or plate length) [m]h convection heat transfer coefficient [W/(m^2*K)]flat_plate_laminar_local_nusseltRex local Reynolds number U x / nuPr Prandtl number of the fluidNux local Nusselt numbernewton_coolingh convection heat transfer coefficient [W/(m^2*K)]A surface area in contact with the fluid [m^2]Ts surface temperature [K]Tinf temperature of the fluid far from the surface [K]q rate of heat transfer [W]prandtl_numbercp specific heat of the fluid [J/(kg*K)]mu dynamic viscosity of the fluid [Pa*s]k thermal conductivity [W/(m*K)]Pr Prandtl number of the fluiddrag_forceCd drag coefficientrho density of the fluid [kg/m^3]v mean flow velocity [m/s]A frontal (reference) area [m^2]F drag force [N]lift_forceCL lift coefficientrho density of the fluid [kg/m^3]v mean flow velocity [m/s]A wing planform area [m^2]F lift force [N]stokes_dragmu dynamic viscosity of the fluid [Pa*s]D sphere diameter [m]v mean flow velocity [m/s]F drag force on the sphere [N]stokes_terminal_velocityg Acceleration [m/s^2] optionalD sphere diameter [m]rho_p density of the particle [kg/m^3]rho density of the fluid [kg/m^3]mu dynamic viscosity of the fluid [Pa*s]v terminal settling velocity [m/s]pin_fin_efficiencyFin efficiency tanh(mL)/(mL) of a cylindrical pin fin with m = sqrt(4h/(kD)).
h heat transfer coefficient [W/(m^2*K)]k fin thermal conductivity [W/(m*K)]D pin diameter [m]L fin length [m]efficiency fin efficiencymL fin parameter m Linfinite_fin_heat_rateh convection heat transfer coefficient [W/(m^2*K)]P perimeter of the fin's cross section [m]k thermal conductivity [W/(m*K)]Ac cross-sectional area of the fin [m^2]Tb temperature at the fin base [K]Tinf temperature of the fluid far from the surface [K]q rate of heat transfer [W]bernoulli_horizontalP1 pressure at the inlet [Pa]rho density of the fluid [kg/m^3]v1 speed at the inlet [m/s]v2 speed at the outlet [m/s]P2 pressure at the outlet [Pa]continuity_speedv1 mean velocity at the inlet [m/s]D1 diameter at the inlet [m]D2 diameter at the outlet [m]v2 mean velocity at the outlet [m/s]dynamic_pressurerho density of the fluid [kg/m^3]v mean flow velocity [m/s]q dynamic pressure [Pa]torricelli_effluxg Acceleration [m/s^2] optionalh depth of the hole below the free surface [m]v speed of the jet leaving the hole [m/s]absolute_pressure_depthP0 pressure at the free surface [Pa]rho density of the fluid [kg/m^3]g Acceleration [m/s^2] optionalh depth below the free surface [m]P absolute pressure at the depth [Pa]buoyant_forcerho density of the fluid [kg/m^3]g Acceleration [m/s^2] optionalV volume of fluid displaced [m^3]F buoyant force [N]hydrostatic_gauge_pressurerho density of the fluid [kg/m^3]g Acceleration [m/s^2] optionalh depth below the free surface [m]P gauge pressure at the depth [Pa]hydrostatic_force_planerho density of the fluid [kg/m^3]g Acceleration [m/s^2] optionalhc depth of the surface's centroid [m]A area of the surface [m^2]F resultant hydrostatic force on the surface [N]compressor_outlet_temperature_airT1 initial temperature [K]P2 final pressure [Pa]P1 initial pressure [Pa]eta isentropic efficiency of the compressorT2 final temperature [K]entropy_change_incompressiblem mass [kg]c specific heat [J/(kg*K)]T2 final temperature [K]T1 initial temperature [K]dS total entropy change [J/K]ideal_gas_lawP absolute pressure of the gas [Pa]V volume of the gas [m^3]n amount of gas [mol]R Gas constant [J/(mol*K)] optionalT absolute temperature [K]entropy_change_ideal_gascp specific heat at constant pressure [J/(kg*K)]R specific gas constant [J/(kg*K)]T1 initial temperature [K]T2 final temperature [K]P1 initial pressure [Pa]P2 final pressure [Pa]ds change in specific entropy [J/(kg*K)]isentropic_temperature_pressure_airT1 initial temperature [K]P2 final pressure [Pa]P1 initial pressure [Pa]T2 final temperature [K]isentropic_temperature_volume_airT1 initial temperature [K]V1 initial volume [m^3]V2 final volume [m^3]T2 final temperature [K]isothermal_work_ideal_gasn amount of gas [mol]R Gas constant [J/(mol*K)] optionalT constant absolute temperature [K]V2 final volume [m^3]V1 initial volume [m^3]W work done by the gas [J]effectiveness_phase_changeN number of transfer units UA/Cmineps heat exchanger effectivenesseffectiveness_parallel_flowN number of transfer units UA/CminCr capacity rate ratio Cmin/Cmaxeps heat exchanger effectivenesssensible_heat_ratemdot mass flow rate of the stream [kg/s]cp specific heat of the fluid [J/(kg*K)]Tout outlet temperature [K]Tin inlet temperature [K]Q rate of heat transfer [W]hx_effectiveness_ntuHeat duty, outlet temperatures, effectiveness and NTU of a counterflow or parallel-flow exchanger.
C_hot heat capacity rate of the hot stream (m cp) [W/K]C_cold heat capacity rate of the cold stream (m cp) [W/K]UA overall conductance U A [W/K]Th_in hot inlet temperature [K]Tc_in cold inlet temperature [K]arrangement flow arrangement choiceQ heat transfer rate [W]Th_out hot outlet temperature [K]Tc_out cold outlet temperature [K]effectiveness effectivenessNTU number of transfer unitsheat_rate_effectivenesseps heat exchanger effectivenessCmin smaller of the two heat capacity rates (m cp) [W/K]Thi inlet temperature of the hot fluid [K]Tci inlet temperature of the cold fluid [K]Q rate of heat transfer [W]lmtdThe LMTD of a counterflow or parallel-flow exchanger from the four terminal temperatures.
Th_in hot stream inlet temperature [K]Th_out hot stream outlet temperature [K]Tc_in cold stream inlet temperature [K]Tc_out cold stream outlet temperature [K]arrangement flow arrangement choicelmtd log-mean temperature difference [K]dT1 temperature difference at the hot-inlet end [K]dT2 temperature difference at the other end [K]ntu_definitionU overall heat transfer coefficient [W/(m^2*K)]A heat transfer area [m^2]Cmin smaller of the two heat capacity rates (m cp) [W/K]N number of transfer units UA/Cmingrashof_numberg Acceleration [m/s^2] optionalbeta volumetric thermal expansion coefficient of the fluid [1/K]Ts surface temperature [K]Tinf temperature of the fluid far from the surface [K]L height of the plate (characteristic length) [m]nu kinematic viscosity of the fluid [m^2/s]Gr Grashof numberrayleigh_numberGr Grashof numberPr Prandtl number of the fluidRa Rayleigh numberfroude_numberv mean flow velocity [m/s]g Acceleration [m/s^2] optionalh flow depth [m]Fr Froude numberblasius_friction_factorRe Reynolds numberf Darcy friction factorcolebrook_friction_factorSolve the implicit Colebrook-White equation for the Darcy friction factor of turbulent pipe flow.
Re Reynolds number (turbulent, at least 4000)eD relative roughness (roughness / diameter)f Darcy friction factorlaminar_friction_factorRe Reynolds numberf Darcy friction factordarcy_weisbach_head_lossf Darcy friction factorL length of the pipe [m]v mean flow velocity [m/s]g Acceleration [m/s^2] optionalD inner diameter of the pipe [m]hL head loss to friction [m]darcy_weisbach_pressure_dropf Darcy friction factorL length of the pipe [m]rho density of the fluid [kg/m^3]v mean flow velocity [m/s]D inner diameter of the pipe [m]dP frictional pressure drop [Pa]haaland_friction_factoreps absolute roughness of the pipe wall [m]D inner diameter of the pipe [m]Re Reynolds numberf Darcy friction factorhagen_poiseuilleD inner diameter of the pipe [m]dP pressure drop along the pipe [Pa]mu dynamic viscosity of the fluid [Pa*s]L length of the pipe [m]Q volume flow rate [m^3/s]kinematic_viscositymu dynamic viscosity of the fluid [Pa*s]rho density of the fluid [kg/m^3]nu kinematic viscosity [m^2/s]minor_loss_headK loss coefficient of the fittingv mean flow velocity [m/s]g Acceleration [m/s^2] optionalhL head loss across the fitting [m]reynolds_numberrho density of the fluid [kg/m^3]v mean flow velocity [m/s]D pipe or body diameter [m]mu dynamic viscosity of the fluid [Pa*s]Re Reynolds numberreynolds_number_kinematicv mean flow velocity [m/s]D pipe or body diameter [m]nu kinematic viscosity of the fluid [m^2/s]Re Reynolds numberswamee_jain_friction_factoreps absolute roughness of the pipe wall [m]D inner diameter of the pipe [m]Re Reynolds numberf Darcy friction factordew_point_temperatureThe temperature at which moist air of a given relative humidity becomes saturated on cooling.
T dry-bulb temperature [K]RH relative humidity (fraction, or % written)T_dew dew-point temperature [K]p_v partial pressure of the water vapour [Pa]humidity_ratio_from_relative_humidityMass of water vapour per kilogram of dry air in moist air of a given relative humidity.
T dry-bulb temperature [K]RH relative humidity (fraction, or % written)P total (barometric) pressure [Pa]W humidity ratio (kg/kg dry air)p_v partial pressure of the water vapour [Pa]humidity_ratio_vapour_pressurepv partial pressure of water vapour [Pa]P total (barometric) pressure of the moist air [Pa]W humidity ratio (kg water vapour per kg dry air)saturation_vapour_pressureThe saturation pressure of water vapour over liquid water (above 0.01 °C) or ice, -100 °C to 200 °C.
T temperature [K]p_sat saturation pressure of water vapour [Pa]moist_air_enthalpyT dry-bulb temperature [K]W humidity ratio (kg water vapour per kg dry air)cpa Specific heat [J/(kg*K)] optionalcpv Specific heat [J/(kg*K)] optionalhg Latent heat [J/kg] optionalT0 Temperature [K] optionalh enthalpy per kilogram of dry air [J/kg]moist_air_specific_volumeT dry-bulb temperature [K]W humidity ratio (kg water vapour per kg dry air)P total (barometric) pressure of the moist air [Pa]Ra Specific gas constant [J/(kg*K)] optionalv specific volume per kilogram of dry air [m^3/kg]wet_bulb_temperatureThe wet-bulb temperature of moist air from its dry-bulb temperature, relative humidity and pressure.
T dry-bulb temperature [K]RH relative humidity (fraction, or % written)P total (barometric) pressure [Pa]T_wb thermodynamic wet-bulb temperature [K]W humidity ratiohydraulic_powerrho density of the fluid [kg/m^3]g Acceleration [m/s^2] optionalQ volume flow rate [m^3/s]H head added by the pump [m]P power delivered to the fluid [W]pump_shaft_powerrho density of the fluid [kg/m^3]g Acceleration [m/s^2] optionalQ volume flow rate [m^3/s]H head added by the pump [m]eta pump efficiency (a fraction)P shaft power required [W]blackbody_emissive_powersigma Stefan boltzmann constant [W/(m^2*K^4)] optionalT absolute temperature of the surface [K]E emissive power per unit area [W/m^2]radiation_heat_transfer_coefficienteps surface emissivitysigma Stefan boltzmann constant [W/(m^2*K^4)] optionalTs surface temperature [K]Tsur temperature of the surroundings [K]hr radiation heat transfer coefficient [W/(m^2*K)]radiation_parallel_platessigma Stefan boltzmann constant [W/(m^2*K^4)] optionalT1 temperature of the first plate [K]T2 temperature of the second plate [K]e1 emissivity of the first platee2 emissivity of the second plateqf net radiative heat flux from plate 1 to plate 2 [W/m^2]radiation_net_exchangeeps emissivity of the surfacesigma Stefan boltzmann constant [W/(m^2*K^4)] optionalA surface area [m^2]Ts surface temperature [K]Tsur temperature of the surroundings [K]q rate of heat transfer [W]wien_displacementT absolute temperature of the surface [K]b Wien constant [m*K] optionallam wavelength of maximum spectral emission [m]carnot_efficiencyTc temperature of the cold reservoir [K]Th temperature of the hot reservoir [K]eta Carnot (maximum) efficiencycarnot_cop_heat_pumpTc temperature of the cold reservoir [K]Th temperature of the hot reservoir [K]cop coefficient of performance (heating)carnot_cop_refrigeratorTc temperature of the cold reservoir [K]Th temperature of the hot reservoir [K]cop coefficient of performance (cooling)brayton_efficiency_airrp compressor pressure ratioeta thermal efficiency of the cyclediesel_efficiency_airr compression ratio V1/V2rc cutoff ratio V3/V2eta thermal efficiency of the cycleotto_efficiency_airr compression ratio V1/V2eta thermal efficiency of the cyclebiot_numberh convection heat transfer coefficient [W/(m^2*K)]Lc characteristic length [m]k thermal conductivity [W/(m*K)]Bi Biot numberfourier_numberalpha thermal diffusivity [m^2/s]t elapsed time [s]Lc characteristic length [m]Fo Fourier numberlumped_capacitance_temperatureTinf temperature of the fluid far from the surface [K]Ti initial temperature of the body [K]h convection heat transfer coefficient [W/(m^2*K)]A surface area of the body [m^2]t elapsed time [s]rho density of the body [kg/m^3]V volume of the body [m^3]c specific heat of the body [J/(kg*K)]T temperature of the body at time t [K]lumped_time_constantrho density of the body [kg/m^3]V volume of the body [m^3]c specific heat of the body [J/(kg*K)]h convection heat transfer coefficient [W/(m^2*K)]A surface area of the body [m^2]tau thermal time constant [s]15 files, 44.2 MB in total. The largest:
| File | Size |
|---|---|
| model.safetensors | 18.9 MB |
| dist/thermofluids_ai999x-1.0.0-py3-none-any.whl | 15 MB |
| onnx/search/encoder.int8.onnx | 4.9 MB |
| docs/thermofluids_ai999x_capabilities.pdf | 4.3 MB |
| onnx/search/index.json | 403.3 KB |
| docs/thermofluids_ai999x_capabilities.html | 289 KB |
| docs/thermofluids_ai999x_capabilities.md | 205.5 KB |
| onnx/search/tokenizer.json | 176.4 KB |
| README.md | 23.6 KB |
| LICENSE | 11.4 KB |
| evaluation/release_gate.md | 2.3 KB |
| evaluation/KNOWLEDGE_CARD.md | 1.5 KB |
Thermofluids answers questions in thermofluids: fluid statics and dynamics, pipe flow, boundary layers, aerodynamics, heat conduction, convection and radiation, heat exchangers, thermodynamic cycles, psychrometrics and combustion. Each answer gives the value with its unit, the steps and the formula in LaTeX.
With pip: pip install thermofluids-ai999x. The same files are on Hugging Face (hf download AI999X/thermofluids-ai999x --local-dir thermofluids-ai999x) and GitHub.
Yes. It is a Python package that runs on an ordinary CPU without a network connection (Python >=3.10); no GPU and no API key are needed.
99 capabilities in 20 topics, including Pipe flow, Convection, Conduction, Gas processes, Heat exchangers.
Field: Engineering. Tasks: Question Answering, Token Classification, Text Classification, Sentence Similarity, Feature Extraction.
Asked "Water with density 998 kg/m^3 and dynamic viscosity 0.001 Pa*s flows at an average velocity of 1.5 m/s in a pipe of diameter 0.05 m. What is the Reynolds number?", it answers: Reynolds number = 74850 1.
It says so and names what is missing or out of range, instead of guessing a number.