[zeinelserfy]

I am trying to model flow over aerofoil using simple foam,after importing geometry and modifying boundary conditions in p & u files and running the case ,i got this message
__________________________________________________ ____________________
Create time

Create mesh for time = 0


SIMPLE: convergence criteria
field p tolerance 1e-05
field U tolerance 1e-05
field nuTilda tolerance 1e-05

Reading field p



--> FOAM FATAL IO ERROR:
"ill defined primitiveEntry starting at keyword 'exit*' on line 29 and ending at line 57"

file: /home/zels496/OpenFOAM-in-Box-18.02/OpenFOAM-dev/tutorials/incompressible/simpleFoam/airFoil2D/airfoiltry/0/p at line 57.

From function void Foam:rimitiveEntry::readEntry(const Foam::dictionary&, Foam::Istream&)
in file db/dictionary/primitiveEntry/primitiveEntryIO.C at line 189.

FOAM exiting
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this is the p file :

/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object p;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

dimensions [0 2 -2 0 0 0 0];

internalField uniform 0;

boundaryField
{
inlet
{
type freestreamPressure;
}
exit
{
type freestreamPressure;
}
top
{
type freestreamPressure;
}
bottom
{
type freestreamPressure;
}
aerofoil
{
type zeroGradient;
}
front
{
type empty;
}
back
{
type empty;
}
}
------------------------------------------------------------------------------------------------------------------
p and u files are uploaded on these links
https://www.4shared.com/file/5SldABKYda/p_online.html
https://www.4shared.com/file/qD7eu3eXda/U_online.html