Документация

open([matlabroot '/toolbox/physmod/simscape/library/m/+foundation/+gas/gas.ssc'])

domain gas
% Gas Domain

% Copyright 2016 The MathWorks, Inc.

parameters
    gas_spec = {1, '1'}; % Gas specification
    %                      1 - Perfect
    %                      2 - Semiperfect
    %                      3 - Real

    % Perfect gas properties

    R      = {0.287,             'kJ/(kg*K)'}; % Specific gas constant
    Z      = {1,                 '1'        }; % Compressibility factor
    T_ref  = {293.15,            'K'        }; % Reference temperature for gas properties
    h_ref  = {420,               'kJ/kg'    }; % Specific enthalpy at reference temperature
    cp_ref = {1,                 'kJ/(kg*K)'}; % Specific heat at constant pressure
    cv_ref = {0.713,             'kJ/(kg*K)'}; % Specific heat at constant volume
    mu_ref = {18,                'uPa*s'    }; % Dynamic viscosity
    k_ref  = {26,                'mW/(m*K)' }; % Thermal conductivity
    Pr_ref = {0.692307692307692, '1'        }; % Prandtl number

    % Semiperfect gas properties

    T_TLU1 = {[150:10:200, 250:50:1000, 1500, 2000]', 'K'}; % Temperature vector

    log_T_TLU1 = {[
        5.01063529409626
        5.07517381523383
        ...
        7.60090245954208
        ], '1'}; % Log temperature vector

    h_TLU1 = {[
        275.264783730547
        285.377054177734
        ...
        2377.14064127409
        ], 'kJ/kg'}; % Specific enthalpy vector

    cp_TLU1 = {[
        1.01211492398124
        1.01042105529234
        ...
        1.24628356718428
        ], 'kJ/(kg*K)'}; % Specific heat at constant pressure vector

    cv_TLU1 = {[
        0.725174216111164
        0.723480347422265
        ...
        0.959342859314206
        ], 'kJ/(kg*K)'}; % Specific heat at constant volume vector

    mu_TLU1 = {[
        10.3766056544352
        10.9908682444892
        ...
        68.0682900809450
        ], 'uPa*s'}; % Dynamic viscosity vector

    k_TLU1 = {[
        14.1517155766309
        15.0474512994325
        ...
        114.486299090693
        ], 'mW/(m*K)'}; % Thermal conductivity vector

    Pr_TLU1 = {[
        0.742123270231960
        0.738025627675206
        ...
        0.740982912785154
        ], '1'}; % Prandtl number vector

    a_TLU1 = {[
        245.095563145758
        253.217606015000
        ...
        863.440849227825
        ], 'm/s'}; % Speed of sound vector

    int_dh_T_TLU1 = {[
        0
        0.0652630980004620
        0.126478959779276
        ...
        2.79681971660776
        ], 'kJ/(kg*K)'}; % integral of dh/T vector

    % Real gas properties

    % Default gas property tables for dry air
    % Rows of the tables correspond to the temperature vector
    % Columns of the tables correspond to the pressure vector

    T_TLU2 = {[150:10:200, 250:50:1000, 1500, 2000]',              'K'  }; % Temperature vector
    p_TLU2 = {[0.01:0.01:0.1, 0.12, 0.15, 0.2, 0.5, 1, 2, 5, 10]', 'MPa'}; % Pressure vector

    log_T_TLU2 = {[
        5.01063529409626
        5.07517381523383
        ...
        7.60090245954208
        ], '1'}; % Log temperature vector

    log_p_TLU2 = {[
        9.21034037197618
        9.90348755253613
        ...
        16.1180956509583
        ], '1'}; % Log pressure vector

    log_rho_TLU2 = {[
        -1.45933859209149 -0.765580954956293 ... 2.84006136461620
        ], '1'}; % Log density table

    s_TLU2 = {[
        3.85666832168988 3.65733557342939 ... 4.66584072487367
        ], 'kJ/(kg*K)'}; % Specific entropy table

    h_TLU2 = {[
        276.007989595737 275.926922934925 ... 2386.79535914098
        ], 'kJ/kg'}; % Specific enthalpy table

    cp_TLU2 = {[
        1.00320557010184 1.00416915257750 ... 1.24767439351222
        ], 'kJ/(kg*K)'}; % Specific heat at constant pressure table

    cv_TLU2 = {[
        0.715425577953031 0.715655648411093	... 0.960303115685940
        ], 'kJ/(kg*K)'}; % Specific heat at constant volume table

    mu_TLU2 = {[
        10.3604759816291 10.3621937105615 ... 68.3249440282350
        ], 'uPa*s'}; % Dynamic viscosity table

    k_TLU2 = {[
        14.0896194596466 14.0962928994967 ... 114.905858092359
        ], 'mW/(m*K)'}; % Thermal conductivity table

    Pr_TLU2 = {[
        0.737684026417089 0.738165370950116 ... 0.741888050943969
        ], '1'}; % Prandtl number table

    a_TLU2 = {[
        245.567929192228 245.496359667264 ... 878.939999571000
        ], 'm/s'}; % Speed of sound table

    log_drho_dp_TLU2 = {[
        -10.6690690699104 -10.6678475863467 ... -13.2956456388403
        ], '1'}; % Log derivative of density with respect to pressure table

    log_drho_dT_TLU2 = {[
        -6.46809263806814 -5.77245144865022 ... -4.77782516923660
        ], '1'}; % Log derivative of density with respect to temperature table

    drhou_dp_TLU2 = {[
        5.41617782089664 5.42024592837099 ... 3.03095417965253
        ], '1'}; % Derivative of internal energy per unit volume with respect to pressure table

    drhou_dT_TLU2 = {[
        -0.195280173069178 -0.391714814336739 ... 1.27305147462835
        ], 'kJ/(m^3*K)'}; % Derivative of internal energy per unit volume with respect to temperature table

    pT_region_flag   = {1,            '1'}; % Valid pressure-temperature region parameterization
    %                                         1 - Range of gas property tables
    %                                         2 - Specified minimum and maximum values
    %                                         3 - Validity matrix
    pT_validity_TLU2 = {ones(24, 18), '1'}; % Pressure-temperature validity matrix

    T_min = {150,  'K'  }; % Minimum valid temperature
    T_max = {2000, 'K'  }; % Maximum valid temperature
    p_min = {0.01, 'MPa'}; % Minimum valid pressure
    p_max = {10,   'MPa'}; % Maximum valid pressure

    p_atm = {0.101325, 'MPa'}; % Atmospheric pressure

    T_unit       = {1, 'K'          }; % Unit for log temperature
    p_unit       = {1, 'Pa'         }; % Unit for log pressure
    rho_unit     = {1, 'kg/m^3'     }; % Unit for log density
    drho_dp_unit = {1, 'kg/(m^3*Pa)'}; % Unit for log derivative of density with respect to pressure
    drho_dT_unit = {1, 'kg/(m^3*K)' }; % Unit for log derivative of density with respect to temperature

    log_ZR = {5.65948221575962, '1'}; % Log of compressibility factor times specific gas constant

    k_cp = {26e-06, 'kg/(m*s)'}; % Ratio of thermal conductivity to specific heat at typical operating conditions

    max_aspect_ratio = {5, '1'}; % Maximum component aspect ratio (length/diameter) for thermal conduction
end

variables
    p = {0.1, 'MPa'}; % Pressure
    T = {300, 'K'  }; % Temperature
end

variables (Balancing=true)
    mdot = {0, 'kg/s'}; % Mass flow rate
    Phi  = {0, 'kW'  }; % Energy flow rate
end

end

foundation.gas.gas