 --------------------------------
 AVL - B O O S T
 Version : v2013.2.0.0.0
 Build:    Nov 11 2013 16:58:06
 System:   ia32-unknown-winnt_i11
 --------------------------------

LICENSE
-------
 Boost Main 2013.0@ License will expire in 240 days

PROJECT
-------
 Preprocessor Version :  2013.2
 Calculation date     : 05.06.2014
 File     : RCCI_new.bst
 Case Set : Case Set
 Case     : Case
 
 Project ID: ""
 Run ID:     ""
 Model date: "11. Dec 2013 10:12:07"

ELEMENTS
--------
 Element Name        Number

 PIPE                   9
 SYSTEMBOUNDARY         2
 PLENUM                 1
 CYLINDER               1
 RESTRICTION            4
 FUELINJECTOR           1
 MEASURINGPOINT         9
 AIRCLEANER             1
 ENGINE                 1
 PIPE_END              20
 ASSEMBLED              1
 ALL_PIPES             10
 ALL_PLENUMS            3
 ALL_BOUNDARIES         2
 RESTRICTIONS           5
 ALL_PIDS               1
 PIPE_VAR_WALL_TEMP    10

GLOBAL DATA
-----------
  Engine Speed :         2000.0  rpm
  Calculationmode:        BOOST  Single
  Cycle Duration:        720.00  degrees
  Max. calc. period:    7200.00  degrees
  Cycles calculated:         10  cycles
  Calc. time steps:     1.00000  degrees (max)
                        1.00000  degrees
                        0.08333  ms
                        0.50000  degrees (short pipe)
                        0.04167  ms (short pipe)
  Traces results step:  3.00000  degrees
  Ref. pressure:      100000.00  Pa
  Ref. temperature:     298.000  K
  Gas properties:      Variable
  General Species Transport Calculation
          Number of Species:       13
          Species No.   1 is: DIESEL
          Species No.   2 is: GASOLINE
          Species No.   3 is: O2
          Species No.   4 is: N2
          Species No.   5 is: H2
          Species No.   6 is: CO2
          Species No.   7 is: H2O
          Species No.   8 is: CO
          Species No.   9 is: O
          Species No.  10 is: NO
          Species No.  11 is: H
          Species No.  12 is: N
          Species No.  13 is: OH
          Multiple Fuel Species:
          Fuel Species No.   1 is: DIESEL                with ratio: 0.999
          Fuel Species No.   2 is: GASOLINE              with ratio: 0.001
  Lower calorific:  0.42803E+08  J/kg
  Stoic. A/F-ratio:      15.169

  Warnings:                   4
  Convergence errors:         0

PIPES
-----

 Total number of pipe cells:     11

 Pipe   Cells   Cell size       W.Heat     Wall T    Fric. coeff.   Lam. Fric. Coeff.  Heat Factor       Volume
  nr.                [mm]         [kJ]        [K]             [-]                 [-]          [-]        [dm3]
    1       1       110.0        0.000     298.00        0.019000           64.000000     1.000000     1.460055
    2       1       120.0        0.000     302.15        0.019000           64.000000     1.000000     0.887626
    3       1       100.0        0.000     302.15        0.019000           64.000000     1.000000     0.145299
    4       1        75.0        0.000     302.15        0.019000           64.000000     1.000000     0.103908
    5       1        75.0        0.000     298.00        0.019000           64.000000     1.000000     0.103908
    6       1        75.0        0.001     360.00        0.019000           64.000000     1.000000     0.086001
    7       1        55.0       -0.003     500.00        0.019000           64.000000     1.000000     0.051426
    8       2        90.0       -0.009     500.00        0.019000           64.000000     1.000000     0.173180
    9       2        85.0       -0.012     450.00        0.019000           64.000000     1.000000     0.163559
   10       1        65.0        0.000     300.00       15.950260       521528.892305     0.000000     0.100000  FILTER_PIPE     1


MEASURINGPOINTS: Average Values
-------------------------------
 Mp. Pipe Location   Diameter  Pressure  Temp. Ms.Temp.  Velo.   Massflow   Massflow To.Ent.f.  To.Ent.f.  Mach. Wtemp.  Converg.
 nr.  nr.     [mm]       [mm]     [bar]    [K]      [K]  [m/s]      [g/s]  [g/cycle]    [kJ/s]  [kJ/cyc.]    [-]    [K]       [-]
  1   1   110.0000   130.0000    1.0300  298.0    298.0    0.5     8.5211     0.5113    -0.001    -0.0001   0.00  298.0 0.134E-05
  2   2   120.0000    44.0000    1.0186  301.1    297.7    4.9     8.5260     0.5116    -0.002    -0.0001   0.01  302.2 0.739E-05
  3   3   100.0000    42.0000    1.0184  301.2    297.5    5.4     8.5248     0.5115    -0.003    -0.0002   0.02  302.2 0.689E-05
  4   4    75.0000    42.0000    1.0183  301.2    297.5    5.4     8.5220     0.5113    -0.002    -0.0001   0.02  302.2 0.761E-05
  5   5    75.0000    42.0000    1.0183  303.1    297.5    5.4     8.5420     0.5125    -0.028    -0.0017   0.02  298.0 0.147E-04
  6   6    75.0000    34.0000    1.0171  309.2    297.9    8.3     8.5326     0.5120    -0.029    -0.0017   0.02  360.0 0.670E-06
  7   7    55.0000    35.0000    1.0104  689.3    784.3   20.1     9.0127     0.5408   -17.046    -1.0228   0.04  500.0 0.385E-05
  8   8   180.0000    35.0000    1.0106  733.7    771.9   19.7     9.0173     0.5410   -17.169    -1.0302   0.04  500.0 0.809E-06
  9   9   170.0000    35.0000    1.0041  766.1    752.4   19.9     9.0175     0.5411   -17.303    -1.0382   0.04  450.0 0.375E-06

SYSTEMBOUNDARIES
Attachments
-----------
 Type                 Nr.   Pipe       Mass flow
                             Nr.       [g/cycle]
 SYSTEMBOUNDARY        1      1          0.5113
 SYSTEMBOUNDARY        2      9          0.5411

PLENUMS: Average Values
-----------------------
                   Pl. Pressure   Temp.      Mass Wallheat
                   nr.    [bar]     [K]       [g]     [kJ]
 PLENUM             1    1.0101  760.96     0.823    0.000
                                          Attached pipe   8:      0.5411 g/cycle
                                          Attached pipe   9:      0.5411 g/cycle
 AIRCLEANER         1    1.0300  298.13     2.157    0.000
                                          Attached pipe   1:      0.5113 g/cycle
                                          Attached pipe  10:      0.5113 g/cycle
 AIRCLEANER         1    1.0193  301.15     1.409    0.000
                                          Attached pipe   2:      0.5116 g/cycle
                                          Attached pipe  10:      0.5113 g/cycle

PLENUMS
Attachments
-----------
 Type                 Nr.   Pipe       Mass flow
                             Nr.       [g/cycle]
 PLENUM                1      8          0.5411
 PLENUM                1      9          0.5411
 AIRCLEANER            1      1          0.5113
 AIRCLEANER            1     10          0.5113
 AIRCLEANER            1      2          0.5116
 AIRCLEANER            1     10          0.5113

CYLINDERS: Average Values
-------------------------
                               Total
                              Engine         Cyl.   1
Firing TDC [deg]                                  0.00
Bore [mm]                                        85.00
Stroke [mm]                                      90.00
Conrodl. [mm]                                   148.00
Piston pin offset [mm]                            0.01
Swept Vol. [l]                   0.5107         0.5107
Compression ratio [-]                            16.10
Dyn. Comp. ratio [-]                             14.74

Combustion Data:
----------------
Combustion Char.                               AVL-MCC     
Comb.start [deg]                                -28.00
Comb.dur.1 [deg]                                156.00
Peak Fir.Pres. [bar]              95.13          95.13
at Crankangle [deg]                8.00           8.00
Peak Pres.Rise[bar/deg]            8.07           8.07
at Crankangle [deg]                2.00           2.00
Peak Fir. Temp. [K]             2268.07        2268.07
at Crankangle [deg]               12.50          12.50
Peak T_burned [K]               2724.39        2724.39
at Crankangle [deg]                4.50           4.50
Res. Gascompr. [bar]               1.06           1.06
at Crankangle [deg]              311.50         311.50

Emissions (Classic Species Transport):
--------------------------------------
NOx: Calculated based on MTZ 34 1973 (12).
CO:  Calculated based on SAE 2002-01-0006.
SOOT:  Calculated based on MTZ 5/2002 (63).
General Species Transport: The emissions results displayed in this section 
are NOT based on the calculated species mass fractions in the cylinder(s).
NOX   [g/kWh]                  10.992232       10.992232
NOX   [g/h]                   80.275850      80.275850
NOX   [ppm]                     2362.04        2362.04
CO    [g/kWh]                  0.038356       0.038356
CO    [g/h]                    0.236995       0.236995
CO    [ppm]                        7.47           7.47
Soot  [g/kWh]                  1.403074       1.403074

Emissions (General Species Transport):
--------------------------------------
The emissions results displayed in this section are the calculated
species mass/mole fractions in the cylinder(s) at End of High Pressure.
 MassFrac DIESEL     [-]       0.002583       0.002583
 MassFrac GASOLINE   [-]       0.000003       0.000003
 MassFrac O2         [-]       0.035253       0.035253
 MassFrac N2         [-]       0.726167       0.726167
 MassFrac H2         [-]       0.000022       0.000022
 MassFrac CO2        [-]       0.159460       0.159460
 MassFrac H2O        [-]       0.075531       0.075531
 MassFrac CO         [-]       0.001474       0.001474
 MassFrac O          [-]       0.000000       0.000000
 MassFrac NO         [-]       0.000000       0.000000
 MassFrac H          [-]       0.000001       0.000001
 MassFrac N          [-]       0.000000       0.000000
 MassFrac OH         [-]       0.000000       0.000000

--------------------------------------
 MoleFrac DIESEL     [-]       0.000738       0.000738
 MoleFrac GASOLINE   [-]       0.000001       0.000001
 MoleFrac O2         [-]       0.031541       0.031541
 MoleFrac N2         [-]       0.742125       0.742125
 MoleFrac H2         [-]       0.000311       0.000311
 MoleFrac CO2        [-]       0.103731       0.103731
 MoleFrac H2O        [-]       0.120030       0.120030
 MoleFrac CO         [-]       0.001506       0.001506
 MoleFrac O          [-]       0.000000       0.000000
 MoleFrac NO         [-]       0.000000       0.000000
 MoleFrac H          [-]       0.000017       0.000017
 MoleFrac N          [-]       0.000000       0.000000
 MoleFrac OH         [-]       0.000000       0.000000

Performance:
------------
IMEP [bar]                       9.0959         9.0959
Rel. to Ave. [-]                                1.0000
IMEP Exh. [bar]                 -1.0470        -1.0470
IMEP Int. [bar]                  0.9053         0.9053
IMEP Gasex. [bar]               -0.1417        -0.1417
IMEP HP [bar]                    9.2377         9.2377
FMEP [bar]                       1.8368         1.8368
BMEP [bar]                       7.2591         7.2591
AMEP;SMEP [bar]                  0.0000         0.0000
ISFC [g/kWh]                   231.8264       231.8264
Rel. to Ave. [-]                                1.0000
ISFC (tr.f.) [g/kWh]           231.8264       231.8264
BSFC [g/kWh]                   290.4878       290.4878
Indicated Eff. [-]               0.3628         0.3628
Iso vol. comb. Eff [-]           0.9620         0.9620
Polytropic Coeff. [-]                           1.3511

Fuel Mass Balance:
------------------
Inj. Fuelmass [g]              0.028450       0.028450
Asp.Trap. Fuelmass [g]         0.001464       0.001464
Fuelmassfl.(A+I) [g/s]         0.498570       0.498570
Fuelmass tot.trap. [g]         0.029914       0.029914
Trapped Fuelm.fl.[g/s]         0.498570       0.498570
Trapp. Eff. Fuel [-]             1.0000         1.0000

Energy Balance Cylinder:
---------------
Fuel Energy [kJ]                1.23416        1.28042
Released Energy [kJ]            1.23416        1.23416
-> Brake Power     [%]           30.039         30.039
-> Loss: Friction  [%]            7.601          7.601
-> Loss: Piston    [%]           16.942         16.942
-> Loss: Head      [%]           13.572         13.572
-> Loss: Liner     [%]            5.285          5.285
-> Loss: Int. Port [%]           -0.212         -0.553
-> Loss: Exh. Port [%]            0.727         -6.524
-> Loss: Exh. Gas  [%]           26.427         26.427
Eff. Rel. Energy [kJ]           1.23416        1.23416
Gross Rel. Energy [kJ]          1.23416        1.23416
Eff.Gross Rel.Ener.[kJ]         1.23416        1.23416
Energy Balance [-]               1.0079         0.9715
Eff. Energy Balance [-]          1.0000         0.9639

Blowby:
-------
Blowbymass [g]                 0.000000       0.000000
Blowbymassfl. [g/s]            0.000000       0.000000
Blowby Heat Flow [kJ]          0.000000       0.000000

Reference Values at SHP:
------------------------
Pressure at SHP[bar]             1.1733         1.1733
Temperature [K]                  366.56         366.56
Air Massfl.  [g/s]             8.504233       8.504233
Fuel Massfl. [g/s]             0.498570       0.498570
Trapp. Eff. Air [-]              1.0025         1.0025
Trapp. Eff.Fuel [-]              1.0000         1.0000
A/F-Ratio (Cmb.) [-]              17.15          17.15
Excess Air Ratio [-]             1.1308         1.1308

Residual Gas:
-------------
Res.gas content [-]              0.0317         0.0317
External EGR [-]                 0.0006         0.0006
Internal EGR [-]                 0.0311         0.0311
Com.Prod.Mass. at EO [g]       0.524125       0.524125
Res.gas mass at SHP [g]        0.016786       0.016786
Res.gas aspirated IN [g]       0.000296       0.000296
Res.gas from intake [g]        0.000296       0.000296
Rel. to Total [-]                0.0177         0.0177
Res.gas flow EX [g]            0.507347       0.507347
Res.gas from exhaust [g]       0.000645       0.000645
Rel. to Total [-]                0.0384         0.0384

Gas Exchange:
-------------
Volumetric Eff. [-]              0.8677         0.8677
Rel. to Ave. [-]                                1.0000
     Rel. To MP 3 [-]            0.8612         0.8612
Total Mass at SHP[g]             0.5298         0.5298
Mass Delivered [g]              0.51197        0.51197
Mass Delivered [g/s]            8.53281        8.53281
Delivery Ratio [-]               0.8685         0.8685
Rel. to Ave. [-]                                1.0000
     Rel. To MP 3 [-]            0.8620         0.8620
Av.Airmass at SHP[g]             0.5131         0.5131
Air Delivered [g]               0.51025        0.51025
Air Delivered [g/s]             8.50423        8.50423
Airdeliveryratio [-]             0.8656         0.8656
Rel. to Ave. [-]                                1.0000
     Rel. To MP 3 [-]            0.8591         0.8591
Airmass Trapped [g]             0.51153        0.51153
Airmass Trapped [g/s]           8.52549        8.52549
Trapp. Eff. Air [-]              1.0025         1.0025
Rel. to Ave. [-]                                1.0000
Airpurity [-]                    0.9685         0.9685
Dyn. Swirl [-]                   0.0000         0.0000
Dyn. Tumble [-]                  0.0000         0.0000

Wall Heatlosses:
----------------
Piston [kJ]                     -0.2091        -0.2091
Cylinderhead [kJ]              -0.16750       -0.16750
Cylinderliner [kJ]             -0.06522       -0.06522
Sum of Wallheat [kJ]           -0.44181       -0.44181
Wall Heatlosses in High Pressure Phase:
Piston HP [kJ]                 -0.20590       -0.20590
Cylinderhead HP [kJ]           -0.16303       -0.16303
Cylinderliner HP [kJ]          -0.04329       -0.04329
Sum of Wallheat HP [kJ]        -0.41222       -0.41222
Wall Heatlosses Related to Heatinput:
Piston [-]                      -0.1633        -0.1633
Cylinderhead [-]                -0.1308        -0.1308
Cylinderliner [-]               -0.0509        -0.0509
Sum of Wallheat [-]             -0.3451        -0.3451
M. Eff. HTC [W/m2/K]             369.89         369.89
M. Eff. Temp. [K]               1272.19        1272.19

Reference Values at EO:
-----------------------
Pressure [bar]                     3.67           3.67
Temperature [K]                 1069.19        1069.19
A/F-Ratio [-]                     16.83          16.83
Com.Prod.Conc. [-]              0.93834        0.93834
Fuel Concentr. [-]             0.002586       0.002586

Average Values of Pipeattachements:
-----------------------------------
 Attached Pipe                                       6
Vlv/Prt.Op.Clr.0mm[deg]                         298.88
Vlv/Prt.Op.Eff.0mm[deg]                         345.26
Vlv/Prt.Op.Eff.1mm[deg]                         370.20
Vlv/Prt.Op.Udef.mm[deg]                         345.26
Vlv/Prt.Cl.Clr.0mm[deg]                         626.12
Vlv/Prt.Cl.Eff.0mm[deg]                         580.56
Vlv/Prt.Cl.Eff.1mm[deg]                         554.64
Vlv/Prt.Cl.Udef.mm[deg]                         580.56
Cam Phasing [deg]                                 0.00
Massflow [g/cycle]                            0.511968
Wallheat [kJ/cycle]                           0.002613
rel.to Heatinp.[-]                              0.0020
 Attached Pipe                                       7
Vlv/Prt.Op.Clr.0mm[deg]                          80.00
Vlv/Prt.Op.Eff.0mm[deg]                         128.00
Vlv/Prt.Op.Eff.1mm[deg]                         153.77
Vlv/Prt.Op.Udef.mm[deg]                         128.00
Vlv/Prt.Cl.Clr.0mm[deg]                         425.00
Vlv/Prt.Cl.Eff.0mm[deg]                         380.57
Vlv/Prt.Cl.Eff.1mm[deg]                         352.79
Vlv/Prt.Cl.Udef.mm[deg]                         380.57
Cam Phasing [deg]                                 0.00
Massflow [g/cycle]                            0.540763
Wallheat [kJ/cycle]                          -0.008973
rel.to Heatinp.[-]                             -0.0070

FLOWRESTRICTIONS: Average Values
--------------------------------
 Flr. Att.Pi.  Massflow  Att.Pi.  Massflow
  nr.  number [g/cycle]   number [g/cycle]
    1       2    0.5118        3    0.5115
    2       3    0.5116        4    0.5113
    3       5    0.5126        6    0.5120
    4       7    0.5410        8    0.5410

FUELINJECTORS: Average Values
-----------------------------
 Inj. Att.Pi.  Massflow  Att.Pi.  Massflow Added Fuel
  nr.  number [g/cycle]   number [g/cycle]  [g/cycle]
    1       4    0.5114        5    0.5125     0.0015

ASSEMBLED: Average Values
-------------------------
 Type         Nr.  ----------Inlet-----------   ---------Outlet-----------    ----------------------Core----------------------
                   Pressure Temperat.   Mass    Pressure Temperat.   Mass     Rej.Heat   Rej.Heat    Fric. coeff.  Heat Factor
                    [bar]     [K]        [g]     [bar]      [K]       [g]       [kJ]       [kW]        [-]           [-]
 AIRCLEANER    1    1.0300   298.13     2.157    1.0193   301.15     1.409     0.0000     0.0000      15.950260     0.000000

ASSEMBLED
Attachments
-----------
 Type                 Nr.   Pipe       Mass flow
                             Nr.       [g/cycle]
 AIRCLEANER            1      1          0.5113
 AIRCLEANER            1      2          0.5116

OVERALL ENGINE PERFORMANCE:
===========================

Indicated Torque          :     36.97 Nm                    Indicated Specific Torque :     72.38 Nm/l
Indicated Power           :      7.74 kW,        10.53 PS   Indicated Specific Power  :     15.16 kW/l,      20.61 PS/l
Friction Torque           :      7.47 Nm                    Friction Power            :      1.56 kW
Effective Torque          :     29.50 Nm                    Effective Specific Torque :     57.77 Nm/l
Effective Power           :      6.18 kW,         8.40 PS   Effective Specific Power  :     12.10 kW/l,      16.45 PS/l

Required time for reading the inputfile and initialisation:       0.00 min
Required time for the calculation: .........................      0.68 min
Required time for writing the outputfile: ..................      0.02 min
Required total time: .......................................      0.70 min
Required total CPU-time: ...................................     41.17 sec
