Gamma = 1.4

Ma = 0.147

ReRef = 110993

Pr = 0.72

GasConstantDim = 287.058

rhoDim = 1.1775

TDim = 418.202

pDim = rhoDim*GasConstantDim*TDim

TwallDim = TDim

Alpha_deg = 0.0

Alpha_rad = Alpha_deg*PI/180

soundSpdDim = sqrt(Gamma*pDim/rhoDim)

L = 1.0

velMagnDim = Ma*soundSpdDim

uDim = velMagnDim*cos(Alpha_rad)

vDim = velMagnDim*sin(Alpha_rad)

muDim = rhoDim*uDim*L/ReRef

Re0 = ReRef/L

rhoInf = rhoDim/rhoDim

uInf = uDim/velMagnDim

vInf = vDim/velMagnDim

pInf = pDim/(rhoDim*velMagnDim*velMagnDim)

Twall = TwallDim/TDim

mu = 1/Re0

GasConstant = GasConstantDim*TDim/(velMagnDim*velMagnDim)

TimeStep = 5e-5

NumSteps = 100000

IO_CheckSteps = 10000

IO_InfoSteps = 1000

IO_CFLSteps = 1000

Skappa = -1.3

Kappa = 0.2

mu0 = 1.0

PreconMatFreezNumb = 1000

NonlinIterTolRelativeL2 = 1.0E-3

LinSysRelativeTolInNonlin = 5.0E-2

NekLinSysMaxIterations = 30

PreconItsStep = 7

rho rhou rhov E C[9,10] C[1] C[5] C[8] C[7] C[6] C[2] C[3] C[4]