[Adlak]

hi everyone,
I want to investigate supersonic combustion in SCRAMJET using
Flamelet combustion model. But rhoReactingFoam is not working well
with it, so I am trying to make Hagen Müller's flameletFoam-2.3.x compatible
with reactingFoam in OpenFoam-2.3.x. I have already investigated
reactingFoam with PaSR combustion model and now looking for
Flamelet combustion model. I have compiled Hagen Müller's flameletFoam with
reactingFoam and it didn't show any error but while running it is
showing following error :

Sum of mass fractions is zero for species
53
(
CH4
CH2O
CH3O
H
O2
H2
O
OH
H2O
HO2
H2O2
C
CH
CH2
CH2(S)
CH3
CO
CO2
HCO
CH2OH
CH3OH
C2H
C2H2
C2H3
C2H4
C2H5
C2H6
HCCO
CH2CO
HCCOH
N
NH
NH2
NH3
NNH
NO
NO2
N2O
HNO
CN
HCN
H2CN
HCNN
HCNO
HOCN
HNCO
NCO
N2
AR
C3H7
C3H8
CH2CHO
CH3CHO
)


From function void
Foam::multiComponentMixture<ThermoType>::correctMa ssFractions()
in file
/home/adlak/Adlak/OpenFOAM/OpenFOAM-2.3.x/OpenFOAM-2.3.x/src/thermophysicalModels/reactionThermo/lnInclude/multiComponentMixture.C
at line 66.

FOAM exiting

*** Error in `flameletFoam': double free or corruption (!prev):
0x0000000001c32560 ***
Aborted (core dumped)

Can anyone help me ??? Please !!!