diff --git a/FSI/flap_perp/SU2-CalculiX/Allclean b/FSI/flap_perp/SU2-CalculiX/Allclean
new file mode 100755
index 000000000..f8286848b
--- /dev/null
+++ b/FSI/flap_perp/SU2-CalculiX/Allclean
@@ -0,0 +1,54 @@
+#!/bin/sh
+cd ${0%/*} || exit 1    # Run from this directory
+
+echo "Cleaning..."
+
+# Participant 1: Fluid
+Participant1="Fluid"
+cd ${Participant1}
+    # Clean the result and auxiliary files
+    rm -fv flow_*.vtk
+    rm -fv history_*.vtk
+    rm -fv restart_flow_*.dat
+    rm -fv forces_breakdown.dat
+    rm -fv surface_flow_*.csv
+cd ..
+
+# Remove the log files
+rm -fv ${Participant1}.log
+
+# Participant 2: Solid
+Participant2="Solid"
+cd ${Participant2}
+    # Clean the case
+    rm -fv *.log
+    rm -fv flap.cvg
+    rm -fv flap.dat
+    rm -fv flap.frd
+    rm -fv flap.sta
+    rm -fv flap.12d
+cd ..
+# Remove the log files
+rm -fv spooles.out
+rm -fv ${Participant2}.log
+
+# Remove the preCICE-related log files
+echo "Deleting the preCICE log files..."
+rm -fv \
+    precice-*.log \
+    precice-postProcessingInfo.log \
+    precice-*-events.json
+    
+# Output files for preCICE versions before 1.2:
+rm -fv \
+    iterations-${Participant1}.txt iterations-${Participant2}.txt \
+    convergence-${Participant1}.txt convergence-${Participant2}.txt \
+    Events-${Participant1}.log Events-${Participant2}.log \
+    EventTimings-${Participant1}.log EventTimings-${Participant2}.log
+
+# Remove the preCICE address files
+rm -rfv precice-run
+rm -fv .*.address
+
+echo "Cleaning complete!"
+#------------------------------------------------------------------------------
diff --git a/FSI/flap_perp/SU2-CalculiX/Allrun b/FSI/flap_perp/SU2-CalculiX/Allrun
new file mode 100755
index 000000000..564f45356
--- /dev/null
+++ b/FSI/flap_perp/SU2-CalculiX/Allrun
@@ -0,0 +1,77 @@
+#!/bin/bash
+
+# This script prepares and runs all the participants in one terminal,
+# forwarding the solvers' output to log files.
+# Alternatively, you may execute the scripts "runSolid" and "runFluid"
+# in separate terminals.
+
+# Run this script with "-parallel" for parallel simulations
+
+# The script "Allclean" cleans-up the result and log files.
+# Set up the run parameters:
+
+# 1 for true, 0 for false
+parallel=0
+if [ "$1" = "-parallel" ]; then
+    parallel=1
+fi
+
+# =============== Participant 1: Fluid ===========================
+Participant1="Fluid"
+Solver1="SU2_CFD"
+nproc=2
+
+# Run and get the process id
+if [ $parallel -eq 1 ]; then
+    echo "  Starting the ${Participant1} participant in parallel..."
+    mpirun -np ${nproc} ${Solver1} Fluid/euler_config_coupled.cfg > ${Participant1}.log 2>&1 &
+else
+    echo "  Starting the ${Participant1} participant in serial..."
+    ${Solver1} Fluid/euler_config_coupled.cfg > ${Participant1}.log 2>&1 &
+fi
+PIDParticipant1=$!
+
+# =============== Participant 2: Solid ===========================
+Participant2="Solid"
+Solver2="ccx_preCICE"
+
+# You can use CalculiX CGX to setup the structural simulation from sratch.
+# This will re-generate the all.msh, fix1_beam.nam, interface_beam.nam files.
+#
+# # Prepare in silent mode
+# echo "Preparing the ${Participant2} participant..."
+# cd ${Participant2}
+#     echo "  Executing cgx (provided by CalculiX, make sure this exists)..."
+#     cgx -bg pre_flap.fbd > prepare_flap.log 2>&1
+# cd ..
+
+# Run
+echo "  Starting the ${Participant2} participant..."
+${Solver2} -i ${Participant2}/flap -precice-participant Calculix > ${Participant2}.log  2>&1 &
+PIDParticipant2=$!
+
+
+# =============== Wait for all the participants to finish =======
+echo "Waiting for the participants to exit..., PIDs: ${PIDParticipant1}, ${PIDParticipant2}"
+echo "(you may run 'tail -f ${Participant1}.log' in another terminal to check the progress)"
+
+echo "To interrupt the simulation, press 'c'. Ctrl+C will only send the processes to the background."
+while [ -e /proc/${PIDParticipant1} ]; do
+    read -r -t1 -n1 input
+    if [ "$input" = "c" ]; then
+        kill ${PIDParticipant1}
+        kill ${PIDParticipant2}
+        false
+    fi
+done
+
+if [ $? -ne 0 ] || [ "$(grep -c -E "error:" ${Participant1}.log)" -ne 0 ] || [ "$(grep -c -E "error:" ${Participant2}.log)" -ne 0 ]; then
+    echo ""
+    echo "Something went wrong... See the log files for more."
+    # Precaution
+    kill ${PIDParticipant1}
+    kill ${PIDParticipant2}
+else
+    echo ""
+    echo "The simulation completed! (check for any errors)"
+fi
diff --git a/FSI/flap_perp/SU2-CalculiX/Fluid/euler_config_coupled.cfg b/FSI/flap_perp/SU2-CalculiX/Fluid/euler_config_coupled.cfg
index 304104c91..6f522fe30 100644
--- a/FSI/flap_perp/SU2-CalculiX/Fluid/euler_config_coupled.cfg
+++ b/FSI/flap_perp/SU2-CalculiX/Fluid/euler_config_coupled.cfg
@@ -212,8 +212,14 @@ SOLUTION_FLOW_FILENAME= Fluid/initial_flow.dat
 % Output file format (PARAVIEW, TECPLOT, STL)
 OUTPUT_FORMAT= PARAVIEW
 %
+% Output file with the forces breakdown
+BREAKDOWN_FILENAME= Fluid/forces_breakdown.dat
+%
+% Output file restart flow
+RESTART_FLOW_FILENAME= Fluid/restart_flow.dat
+%
 % Output file convergence history (w/o extension)
-CONV_FILENAME= history
+CONV_FILENAME= Fluid/history
 %
 % Write binary restart files (YES, NO)
 WRT_BINARY_RESTART= NO
@@ -222,7 +228,10 @@ WRT_BINARY_RESTART= NO
 READ_BINARY_RESTART= NO
 %
 % Output file flow (w/o extension) variables
-VOLUME_FLOW_FILENAME= flow
+VOLUME_FLOW_FILENAME= Fluid/flow
+%
+% Output file surface flow coefficient (w/o extension)
+SURFACE_FLOW_FILENAME= Fluid/surface_flow
 %
 % Write surface solution files
 WRT_SRF_SOL= NO
diff --git a/FSI/flap_perp/SU2-CalculiX/Fluid/euler_config_coupled_mergeSolution.cfg b/FSI/flap_perp/SU2-CalculiX/Fluid/euler_config_coupled_mergeSolution.cfg
deleted file mode 100644
index 7847e818b..000000000
--- a/FSI/flap_perp/SU2-CalculiX/Fluid/euler_config_coupled_mergeSolution.cfg
+++ /dev/null
@@ -1,267 +0,0 @@
-%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-%                                                                              %
-% SU2 configuration file                                                       %
-% Case description: Coupled FSI simulation of fluid flow over a flap           %
-% Authors: Kirill Martynov, Dmytro Sashko, Jan Sültemeyer                      %
-% Institution: Technische Universität München                                  %
-% Date: 01.11.2017                                                             %
-%                                                                              %
-%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-
-% ------------- PRECICE PROBLEM DEFINITION ------------%
-
-PRECICE_USAGE= YES
-%
-PRECICE_CONFIG_FILENAME= ./precice-config.xml
-%
-PRECICE_WETSURFACE_MARKER_NAME= wetSurface
-%
-PRECICE_NUMBER_OF_WETSURFACES= 1
-
-% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
-
-% Physical governing equations (EULER, NAVIER_STOKES, NS_PLASMA)
-PHYSICAL_PROBLEM= EULER
-%
-% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
-MATH_PROBLEM= DIRECT
-%
-% Restart solution (NO, YES)
-RESTART_SOL= YES
-
-% -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
-
-% Mach number (non-dimensional, based on the free-stream values)
-MACH_NUMBER= 0.01
-%
-% Angle of attack (degrees, only for compressible flows)
-AOA= 0.0
-%
-% Side-slip angle (degrees, only for compressible flows)
-SIDESLIP_ANGLE= 0.0
-%
-% Free-stream pressure (101325.0 N/m^2 by default)  
-FREESTREAM_PRESSURE= 101300.0
-%
-% Free-stream temperature (288.15 K by default)
-FREESTREAM_TEMPERATURE= 288.0
-
-% ------------------------- UNSTEADY SIMULATION -------------------------------%
-
-% Unsteady simulation (NO, TIME_STEPPING, DUAL_TIME_STEPPING-1ST_ORDER,
-%                      DUAL_TIME_STEPPING-2ND_ORDER, TIME_SPECTRAL)
-UNSTEADY_SIMULATION= DUAL_TIME_STEPPING-1ST_ORDER
-%
-% Time Step for dual time stepping simulations (s)
-UNST_TIMESTEP= 0.01
-%
-% Total Physical Time for dual time stepping simulations (s)
-UNST_TIME= 4.01
-%
-% Number of internal iterations (dual time method)
-UNST_INT_ITER= 200
-%
-% Iteration number to begin unsteady restarts
-UNST_RESTART_ITER= 1
-
-% ----------------------- DYNAMIC MESH DEFINITION -----------------------------%
-
-% Dynamic mesh simulation (NO, YES)
-GRID_MOVEMENT= YES
-%
-% Type of dynamic mesh (NONE, RIGID_MOTION, DEFORMING, ROTATING_FRAME,
-%                       MOVING_WALL, STEADY_TRANSLATION, FLUID_STRUCTURE,
-%                       AEROELASTIC, ELASTICITY, EXTERNAL,
-%                       AEROELASTIC_RIGID_MOTION, GUST, PRECICE_MOVEMENT)
-GRID_MOVEMENT_KIND= PRECICE_MOVEMENT
-%
-% Moving wall boundary marker(s) (NONE = no marker, ignored for RIGID_MOTION)
-MARKER_MOVING= ( wetSurface0 )
-
-% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
-
-% Euler wall boundary marker(s) (NONE = no marker)
-MARKER_EULER= ( upper_wall, lower_wall, wetSurface0 )
-%
-% Inlet boundary marker(s) (NONE = no marker) 
-% Format: ( inlet marker, total temperature, total pressure, flow_direction_x, 
-%           flow_direction_y, flow_direction_z, ... ) where flow_direction is
-%           a unit vector.
-MARKER_INLET= ( inlet, 288.6, 101400.0, 1.0, 0.0, 0.0 )
-%
-% Outlet boundary marker(s) (NONE = no marker)
-% Format: ( outlet marker, back pressure (static), ... )
-MARKER_OUTLET= ( outlet, 101300.0 )
-%
-% Symmetry boundary marker for quasi-2D simulation 
-MARKER_SYM = ( symmetry )
-
-% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
-
-% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
-NUM_METHOD_GRAD= GREEN_GAUSS
-%
-% Courant-Friedrichs-Lewy condition of the finest grid
-CFL_NUMBER= 2.0
-%
-% Adaptive CFL number (NO, YES)
-CFL_ADAPT= NO
-%
-% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
-%                                        CFL max value )
-CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
-%
-% Runge-Kutta alpha coefficients
-RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-%
-% Number of total iterations
-EXT_ITER= 999999
-
-% ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
-
-% Linear solver for implicit formulations (BCGSTAB, FGMRES)
-LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
-LINEAR_SOLVER_PREC= LU_SGS
-%
-% Minimum error of the linear solver for implicit formulations
-LINEAR_SOLVER_ERROR= 1E-4
-%
-% Max number of iterations of the linear solver for the implicit formulation
-LINEAR_SOLVER_ITER= 20
-
-% -------------------------- MULTIGRID PARAMETERS -----------------------------%
-
-% Multi-Grid Levels (0 = no multi-grid)
-MGLEVEL= 3
-%
-% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
-MGCYCLE= V_CYCLE
-%
-% Multi-grid pre-smoothing level
-MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
-%
-% Multi-grid post-smoothing level
-MG_POST_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Jacobi implicit smoothing of the correction
-MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
-%
-% Damping factor for the residual restriction
-MG_DAMP_RESTRICTION= 0.9
-%
-% Damping factor for the correction prolongation
-MG_DAMP_PROLONGATION= 0.9
-
-% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
-
-% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
-%                              TURKEL_PREC, MSW)
-CONV_NUM_METHOD_FLOW= JST
-%
-% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
-%           Required for 2nd order upwind schemes (NO, YES)
-MUSCL_FLOW= YES
-%
-% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG,
-%                BARTH_JESPERSEN, VAN_ALBADA_EDGE)
-SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
-%
-% Coefficient for the Venkat's limiter (upwind scheme). A larger values decrease
-%             the extent of limiting, values approaching zero cause
-%             lower-order approximation to the solution (0.05 by default)
-VENKAT_LIMITER_COEFF= 0.05
-%
-% 2nd and 4th order artificial dissipation coefficients for
-%     the JST method ( 0.5, 0.02 by default )
-JST_SENSOR_COEFF= ( 0.5, 0.02 )
-%
-% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
-TIME_DISCRE_FLOW= EULER_IMPLICIT
-
-% --------------------------- CONVERGENCE PARAMETERS --------------------------%
-
-% Convergence criteria (CAUCHY, RESIDUAL)
-%
-CONV_CRITERIA= RESIDUAL
-%
-% Residual reduction (order of magnitude with respect to the initial value)
-RESIDUAL_REDUCTION= 1
-%
-% Min value of the residual (log10 of the residual)
-RESIDUAL_MINVAL= -3.5
-%
-% Start convergence criteria at iteration number
-STARTCONV_ITER= 10
-
-% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
-
-% Write residuals
-WRT_RESIDUALS= YES
-%
-% Mesh input file
-MESH_FILENAME= Fluid/fluidMesh.su2
-%
-% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
-MESH_FORMAT= SU2
-%
-% Restart flow input file
-SOLUTION_FLOW_FILENAME= Fluid/restart_flow.dat
-%
-% Output file format (PARAVIEW, TECPLOT, STL)
-OUTPUT_FORMAT= PARAVIEW
-%
-% Output file convergence history (w/o extension)
-CONV_FILENAME= history
-%
-% Write binary restart files (YES, NO)
-WRT_BINARY_RESTART= NO
-%
-% Read binary restart files (YES, NO)
-READ_BINARY_RESTART= NO
-%
-% Output file flow (w/o extension) variables
-VOLUME_FLOW_FILENAME= flow
-%
-% Write surface solution files
-WRT_SRF_SOL= NO
-%
-% Writing solution file frequency
-WRT_SOL_FREQ= 1
-%
-% Writing solution file frequency for physical time steps (dual time)
-WRT_SOL_FREQ_DUALTIME= 1
-%
-% Writing convergence history frequency
-WRT_CON_FREQ= 1
-%
-% Writing convergence history frequency
-WRT_CON_FREQ_DUALTIME= 1
-
-% ------------------------ GRID DEFORMATION PARAMETERS ------------------------%
-%
-% Linear solver or smoother for implicit formulations (FGMRES, RESTARTED_FGMRES, BCGSTAB)
-DEFORM_LINEAR_SOLVER= FGMRES
-%
-% Preconditioner of the Krylov linear solver (ILU, LU_SGS, JACOBI)
-DEFORM_LINEAR_SOLVER_PREC= LU_SGS
-%
-% Number of smoothing iterations for mesh deformation
-DEFORM_LINEAR_ITER= 50
-%
-% Number of nonlinear deformation iterations (surface deformation increments)
-DEFORM_NONLINEAR_ITER= 1
-%
-% Print the residuals during mesh deformation to the console (YES, NO)
-%DEFORM_CONSOLE_OUTPUT= NO
-%
-% Factor to multiply smallest cell volume for deform tolerance (0.001 default)
-DEFORM_TOL_FACTOR = 0.1
-%
-% Type of element stiffness imposed for FEA mesh deformation (INVERSE_VOLUME,
-%                                          WALL_DISTANCE, CONSTANT_STIFFNESS)
-DEFORM_STIFFNESS_TYPE= INVERSE_VOLUME
-%
-% Visualize the deformation (NO, YES)
-%VISUALIZE_DEFORMATION= YES
diff --git a/FSI/flap_perp/SU2-CalculiX/README.md b/FSI/flap_perp/SU2-CalculiX/README.md
index 6e2b9135a..e95f34ec0 100644
--- a/FSI/flap_perp/SU2-CalculiX/README.md
+++ b/FSI/flap_perp/SU2-CalculiX/README.md
@@ -1,3 +1,7 @@
-# Tutorial for a coupled simulation with SU2 and CalculiX
+# Tutorial for an FSI simulation of an elastic flap perpendicular to a channel flow using SU2 and CalculiX
 
-The files in this folder can be used to run the tutorial test case described on this [Wiki page](https://github.com/precice/precice/wiki/FSI-tutorial). For running the case either follow the instructions given there or execute the script `runTutorial_serial.sh` or `runTutorial_parallel.sh` (with SU2 being executed with one or several processes, respectively).
+This tutorial is described in the [preCICE wiki](https://github.com/precice/precice/wiki/FSI-tutorial).
+
+You may run the coupled simulation in serial using the script `Allrun` or in parallel with `Allrun -parallel`. The output of each step will be redirected to log files (mainly `Fluid.log` and `Solid.log`). You can cleanup the simulation using `Allclean`.
+
+If you prefer to run the two simulations in two different terminals and watch their output on the screen, use the (simpler) scripts `runFluid` (or `runFluid -parallel`) and `runSolid`. They also write the output to the same log files.
diff --git a/FSI/flap_perp/SU2-CalculiX/plotDisplacement.sh b/FSI/flap_perp/SU2-CalculiX/plotDisplacement.sh
index 6ccc0bb84..62a27931b 100755
--- a/FSI/flap_perp/SU2-CalculiX/plotDisplacement.sh
+++ b/FSI/flap_perp/SU2-CalculiX/plotDisplacement.sh
@@ -4,5 +4,5 @@ set grid
 set title 'Displacement of the Flap Tip'
 set xlabel 'Time [s]'
 set ylabel 'X-Displacement [m]'
-plot "point1.watchpoint.txt" using 1:5 smooth cumulative title ""
+plot "precice-Calculix-watchpoint-point1.log" using 1:5 smooth cumulative title ""
 EOF
diff --git a/FSI/flap_perp/SU2-CalculiX/precice-config.xml b/FSI/flap_perp/SU2-CalculiX/precice-config.xml
index f92b97a05..80a333be8 100644
--- a/FSI/flap_perp/SU2-CalculiX/precice-config.xml
+++ b/FSI/flap_perp/SU2-CalculiX/precice-config.xml
@@ -40,7 +40,7 @@
         <watch-point mesh="Calculix_Mesh" name="point1" coordinate="-0.05;0.01;1" />
       </participant>
 
-      <m2n:sockets from="SU2_CFD" to="Calculix"  exchange-directory="../" />
+      <m2n:sockets from="SU2_CFD" to="Calculix" />
       
       <coupling-scheme:parallel-implicit>
       <!--coupling-scheme:serial-implicit-->
diff --git a/FSI/flap_perp/SU2-CalculiX/runFluid b/FSI/flap_perp/SU2-CalculiX/runFluid
new file mode 100755
index 000000000..7527d01a6
--- /dev/null
+++ b/FSI/flap_perp/SU2-CalculiX/runFluid
@@ -0,0 +1,25 @@
+#!/bin/bash
+
+# Fluid participant
+
+# Run this script in one terminal and the "runSolid" script in another terminal.
+# These scripts present how the two participants would be started manually.
+# Alternatively, you may execute the "Allrun" script in one terminal.
+
+# Run this script with "-parallel" for parallel simulations
+
+# The script "Allclean" cleans-up the result and log files.
+
+# 1 for true, 0 for false
+parallel=0
+if [ "$1" = "-parallel" ]; then
+    parallel=1
+fi
+
+echo "Preparing and running the Fluid participant..."
+
+if [ $parallel -eq 1 ]; then
+    mpirun -n 2 SU2_CFD Fluid/euler_config_coupled.cfg 2>&1 | tee Fluid.log
+else
+    SU2_CFD Fluid/euler_config_coupled.cfg 2>&1 | tee Fluid.log
+fi
diff --git a/FSI/flap_perp/SU2-CalculiX/runSolid b/FSI/flap_perp/SU2-CalculiX/runSolid
new file mode 100755
index 000000000..2d2f2ec08
--- /dev/null
+++ b/FSI/flap_perp/SU2-CalculiX/runSolid
@@ -0,0 +1,14 @@
+#!/bin/bash
+
+# Solid participant
+
+# Run this script in one terminal and the "runFluid" script in another terminal.
+# These scripts present how the two participants would be started manually.
+# Alternatively, you may execute the "Allrun" script in one terminal.
+
+# The script "Allclean" cleans-up the result and log files.
+
+echo "Running the Solid participant..."
+
+# Run
+ccx_preCICE -i Solid/flap -precice-participant Calculix 2>&1 | tee Solid.log
diff --git a/FSI/flap_perp/SU2-CalculiX/runTutorial_parallel.sh b/FSI/flap_perp/SU2-CalculiX/runTutorial_parallel.sh
deleted file mode 100755
index 2d329f9a2..000000000
--- a/FSI/flap_perp/SU2-CalculiX/runTutorial_parallel.sh
+++ /dev/null
@@ -1,48 +0,0 @@
-#! /bin/bash 
-
-
-tmux has-session -t PreciceSU2-Calculix-newtonParallel 2>/dev/null
-if [ "$?" -eq 1 ] ; then 
-    tmux new-session -d -s 'PreciceSU2-Calculix-newtonParallel'
-    tmux split-window -v
-fi
-
-
-session=PreciceSU2-Calculix-newtonParallel
-window=${session}:0
-pane_su2=${window}.0
-pane_Calculix=${window}.1
-tmux send-keys -t "$pane_su2" C-z '( time mpirun -n 2 SU2_CFD Fluid/euler_config_coupled.cfg ) 2>&1  | tee Su2.log' Enter
-tmux select-pane -t "$pane_su2"
-tmux select-window -t "$window"
-tmux send-keys -t "$pane_Calculix" C-z '( time ccx_preCICE -i Solid/flap -precice-participant  Calculix ) 2>&1  | tee Calculix.log' Enter 
-tmux select-pane -t "$pane_Calculix"
-tmux select-window -t "$window"
-tmux attach-session -t "$session"
-
-tmux detach -s "$session" 
-
-SU2_SOL Fluid/euler_config_coupled_mergeSolution.cfg
-
-rm -rf Output
-mkdir Output
-cp flow*.vtk Output
-cp euler_config_coupled.cfg Output
-cp flap.inp Output
-cp Calculix.log Output
-cp Su2.log Output
-cp precice-config.xml Output
-cp point1.watchpoint.txt Output
-cp plotDisplacement.sh Output
-# clean everything 
-rm -f *log
-rm -f *vtk
-rm -f *txt
-rm -f *csv
-rm -f *out
-rm -f restart_flow*
-rm -f forces*
-rm -f flap.[^i]*
-
- echo " Copying of results was successfull! Let's hope that simulation went well as well. Results are in the output
- folder" 
diff --git a/FSI/flap_perp/SU2-CalculiX/runTutorial_serial.sh b/FSI/flap_perp/SU2-CalculiX/runTutorial_serial.sh
deleted file mode 100755
index de486e22d..000000000
--- a/FSI/flap_perp/SU2-CalculiX/runTutorial_serial.sh
+++ /dev/null
@@ -1,46 +0,0 @@
-#! /bin/bash 
-
-
-tmux has-session -t PreciceSU2-Calculix-newtonParallel 2>/dev/null
-if [ "$?" -eq 1 ] ; then 
-    tmux new-session -d -s 'PreciceSU2-Calculix-newtonParallel'
-    tmux split-window -v
-fi
-
-
-session=PreciceSU2-Calculix-newtonParallel
-window=${session}:0
-pane_su2=${window}.0
-pane_Calculix=${window}.1
-tmux send-keys -t "$pane_su2" C-z '( time SU2_CFD Fluid/euler_config_coupled.cfg ) 2>&1  | tee Su2.log' Enter
-tmux select-pane -t "$pane_su2"
-tmux select-window -t "$window"
-tmux send-keys -t "$pane_Calculix" C-z '( time ccx_preCICE -i Solid/flap -precice-participant Calculix ) 2>&1  | tee Calculix.log' Enter 
-tmux select-pane -t "$pane_Calculix"
-tmux select-window -t "$window"
-tmux attach-session -t "$session"
-
-tmux detach -s "$session" 
-
-rm -rf Output
-mkdir Output
-cp flow*.vtk Output
-cp euler_config_coupled.cfg Output
-cp flap.inp Output
-cp Calculix.log Output
-cp Su2.log Output
-cp precice-config.xml Output
-cp point1.watchpoint.txt Output
-cp plotDisplacement.sh Output
-# clean everything 
-rm -f *log
-rm -f *vtk
-rm -f *txt
-rm -f *csv
-rm -f *out
-rm -f restart_flow*
-rm -f forces*
-rm -f flap.[^i]*
-
- echo " Copying of results was successfull! Let's hope that simulation went well as well. Results are in the output
- folder"