From 3e3ebb7f61eeb89811ed980f6f40e89691b6a977 Mon Sep 17 00:00:00 2001 From: Alfonso Date: Wed, 13 Feb 2019 17:56:34 +0000 Subject: [PATCH] Minor syntax modifications --- src/lowOrder2D/calcs.jl | 2 -- src/lowOrder2D/solvers.jl | 2 +- src/lowOrder2D/typedefs.jl | 3 +-- src/utils.jl | 2 -- 4 files changed, 2 insertions(+), 7 deletions(-) diff --git a/src/lowOrder2D/calcs.jl b/src/lowOrder2D/calcs.jl index 3f37d60f..92b05eba 100755 --- a/src/lowOrder2D/calcs.jl +++ b/src/lowOrder2D/calcs.jl @@ -193,8 +193,6 @@ function update_bv(surf::TwoDSurf) gamma[ib] = gamma[ib]*surf.uref*surf.c end - - for ib = 2:surf.ndiv surf.bv[ib-1].s = (gamma[ib]+gamma[ib-1])*(surf.theta[2]-surf.theta[1])/2. surf.bv[ib-1].x = (surf.bnd_x[ib] + surf.bnd_x[ib-1])/2. diff --git a/src/lowOrder2D/solvers.jl b/src/lowOrder2D/solvers.jl index c9b9639d..ee951f65 100755 --- a/src/lowOrder2D/solvers.jl +++ b/src/lowOrder2D/solvers.jl @@ -205,7 +205,7 @@ function ldvm(surf::TwoDSurf, curfield::TwoDFlowField, nsteps::Int64 = 500, dtst lesp = surf.a0[1] #Check for LESP condition - if (abs(lesp)>surf.lespcrit[1]) + if abs(lesp)>surf.lespcrit[1] #2D iteration if LESP_crit is exceeded #Add a LEV with dummy strength diff --git a/src/lowOrder2D/typedefs.jl b/src/lowOrder2D/typedefs.jl index 5a402f3d..fa16359a 100755 --- a/src/lowOrder2D/typedefs.jl +++ b/src/lowOrder2D/typedefs.jl @@ -107,11 +107,10 @@ struct TwoDSurf if (typeof(kindef.h) == EldUpDef) kinem.h = kindef.h(0.)*c kinem.hdot = ForwardDiff.derivative(kindef.h,0.)*uref - elseif (typeof(kindef.h) == EldUpIntDef) + elseif (typeof(kindef.h) == EldUpIntDef) kinem.h = kindef.h(0.)*c kinem.hdot = ForwardDiff.derivative(kindef.h,0.)*uref elseif (typeof(kindef.h) == EldRampReturnDef) - kinem.h= kindef.h(0.)*c kinem.hdot = ForwardDiff.derivative(kindef.h,0.)*uref elseif (typeof(kindef.h) == ConstDef) diff --git a/src/utils.jl b/src/utils.jl index 49c2363e..9c98fb45 100755 --- a/src/utils.jl +++ b/src/utils.jl @@ -104,7 +104,6 @@ function camber_calc(x::Vector,airfoil::String) ndiv = length(x); c = x[ndiv]; - cam = zeros(ndiv) cam_slope = zeros(ndiv) in_air = DelimitedFiles.readdlm(airfoil, Float64); @@ -113,7 +112,6 @@ function camber_calc(x::Vector,airfoil::String) ncoord = length(xcoord); xcoord_sum = zeros(ncoord); - xcoord_sum[1] = 0; for i = 1:ncoord-1 xcoord_sum[i+1] = xcoord_sum[i] + abs(xcoord[i+1]-xcoord[i]); end