Free software download (R)

Free software download

GNU Licence Agreement

You have to be registered and logged in to download free software.

Name

Annotation

Files to download

Software vdK 1.1.3.4

Software evaluates the crack growth measurements to obtain the influence of crack growth rate on the range of stress intensity factor for the central notch specimens.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software

User manual

SAAD software

Statistical processing and evaluation of aerodynamic data computed by the CFD solver EDGE.

This project result was developed within the VG20102014052 project “Automated aerial information system (2010-2014, MV0/VG)“ provider MV.

software

User manual

Software AE v.2011

Software evaluates measured acoustic emission signals in order to obtain time charts and approximate localization of developed defects in test specimen.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software

User manual

Software JINT 2011

Software evaluates the measuring of F=F(COD) dependence of CT specimen to fracture toughness computed as stress intensity factor and J-Integral.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software

User manual

POLAR_ALFA and POLAR_BETA programmes

Polar_alfa and polar_beta programmes are used for settiing of input CFD data of EDGE software. The data are changed in the given range of angle of attack and side slip angle, automatically. Polar_beta program is using for sideslip flight regime. Programme was created in MATLAB and enables to overwrite the input files for individual angles of attack. Programme is launched at OCTAVE with command polar_alfa or polar_beta respectively. User set the free stream speed only. Wanted Angles of attack are set directly in m.file. After computation cycle the programme save the output to TECPLOT and launch next calculation cycle. Program enable to compute polar curve, without to overwrite input file in each step of the calculation, that leads to short the computation process and error elimination in setting the input file.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software

User manual

WTMC-view software

Program WTMC-view is determined for creating, depiction and saving combinations of graphs of aircraft model windtunnel measurements. Inputs are list of measurements with values of measured configuration parameters and measurement data files. List of combinations can by created directly in program by designated constant and variable configuration parameters. List can by also loaded from text file, series of graphs are subsequently saved. Program is suitable for final analysis of large set of measurements.

This research plan result was developed within MSM0001066901 institutional research plan  "External aerodynamics development (2004-2010, MSM)" provider MŠMT.

software

User manual

SAD software

Software SAD determine static aerodynamic derivatives from aircraft model wind tunnel measurements. Inputs are measurement data files and list of measurement files and deflections. Program enable edit, depict and save graphic and text output files.

This research plan result was developed within MSM0001066901 institutional research plan  "External aerodynamics development (2004-2010, MSM)" provider MŠMT.

software

User manual

JetNoise software

A software for a numerical prediction of a noise generation from air nozzles. The software is based on the Goldstein acoustic model for axisymmetrical jets. The flow variables needed by the acoustic model are computed by RANS equations for an axisymmetric problem.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software

User manual

URANS3DMBI

Software is designated for calculation of the unsteady three-dimensional inviscid compressible flow in the stator-rotor system of the axial turbine stage.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software

User manual

Wingload2 software

Wingload2 is a software for calculation of elastic slender wings loading.

This project result was developed within the  FR-TI1/326 project “FTG - New Generation Fiberglass Two-seater Glider (2009-2013, MPO/FR)“ provider MPO.

software

User manual

Wingload1 software

Wingload1 is a software intended for calculation of loading of slender rigid wings.

This research plan result was developed within MSM0001066901 institutional research plan  "External aerodynamics development (2004-2010, MSM)" provider MŠMT.

software

User manual

OPTKLAPKA software version 2011

Software package OPTKLAPKA is a universal optimizer of
aerodynamic flaps.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software

User manual

OPTKRIDLO software version 2010

Software package OPTKRIDLO is a universal optimizer of
aerodynamic wings. It contains a package for parameterization of wings, a package for their evaluation and the evolutionary algorithm.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software

User manual

OPTPROFIL software version 2010

Software package OPTPROFIL is a universal optimizer of airfoils consisting of the airfoil-evaluation package, airfoil-parameterization package, and a mutli-objective evolutionary algorithm.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software

User manual

MIARMOGA software version 2011

Package MIARMOGA contains the multi-objective micro-genetic
algorithm with range-adaptation with new improved procedures.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software

User manual

Software WARMBLADE

Software for calculation of the temperature field for two-dimensional compressible turbulent flow past blade cascade. The temperature field is calculated in both parts: in fluid and inside the blade.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software

User manual

 ADD software

The ADD program is used for estimation of aerodynamic damping derivative from wind tunnel measurement. It is created in Matlab and run is done in this simulation program. The principle of determining the damping derivatives is based on an estimate of the angular rate and damping of exponential signal.

This project result was developed within the VG20102014052 project “Automated aerial information system (2010-2014, MV0/VG)“ provider MV.

software

User manual

CalcMatrix_96_1

The program is used to calculate the calibration matrix of third order for the six component balance. The calculated calibration matrix has a size of 6x96.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software

User manual

QUEUE software

Queue is a software for gradual processing of commands in the command line.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software

User manual

Software STARES

An interactive software to evaluate the statistical values of the last iterations of the calculations.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software

User manual

External calibration of load cell

Software enables calibration of load cells out of laboratory. The software calculates and evaluates measured data.

This research plan result was developed within MSM0001066903 institutional research plan  "Research of strength of low-weight structures with special regard to airplane structures (2004-2010, MSM)" provider MŠMT.

software

User manual

Program NLWING2 for viscous analysis of slim wings

NLWING2 is an implementation of the nonlinear lifting-line method developed at VZLÚ. It enables utilization of the results of either nonviscous or viscous 2D analysis of airfoils for investigation of 3D configurations of slim wings.

This research plan result was developed within MSM0001066901 institutional research plan  "External aerodynamics development (2004-2010, MSM)" provider MŠMT.

software

User manual

PYTAVE 2

Pytave 2 is an extending package for the Python programming language, enabling merging of the GNU Octave computing environment and using its functions from Python.

This research plan result was developed within MSM0001066901 institutional research plan  "External aerodynamics development (2004-2010, MSM)" provider MŠMT.

software

user manual

GNU OCTAVE 3.2.4

GNU OCTAVE 3.2.4 is an interpreter of a programming language and computing environment for general numerical computations. It is to a high degree compatible with MATLAB.

This research plan result was developed within MSM0001066901 institutional research plan  "External aerodynamics development (2004-2010, MSM)" provider MŠMT.

software

user manual

XFEVAL module for automatization of computations by the XFOIL-programme

XFEVAL is a modul for the scripting language Python for effective automatic optimizations of aerodynamic airfoils by using the XFOIL-programme.

This research plan result was developed within MSM0001066901 institutional research plan  "External aerodynamics development (2004-2010, MSM)" provider MŠMT.

software

user manual

Programmes for working with the GPARSEC parameterization

The GPARSEC parameterization is intended for digitalization of subsonic aerodynamic airfoils by using its important geometric characteristics with straightforward physical meaning.

This research plan result was developed within MSM0001066901 institutional research plan  "External aerodynamics development (2004-2010, MSM)" provider MŠMT.

software

user manual

MEAF

MEAF is a software for generation of 2D meshes around multielement airfoils. These meshes are composed of structured parts around airfoil for capturing boundary layer and of remaining triangle mesh. Output format of meshes is FFA, CGNS and GNUPLot.

This research plan result was developed within MSM0001066901 institutional research plan  "External aerodynamics development (2004-2010, MSM)" provider MŠMT.

software (for linux)

user manual

MIARMOGA2

The package MIARMOGA2 is a completely reworked version of MIARMOGA immersed into the GNU Octave universal computing system with an aim to supersede its predecessor. MIARMOGA2 has several new interesting features to offer.

This research plan result was developed within MSM0001066901 institutional research plan  "External aerodynamics development (2004-2010, MSM)" provider MŠMT.

software

user manual

MIARMOGA version 2010

MIARMOGA version 2010 is the up-to-date version of the well established multi-objective microgenetic algorithm with range adaptation. The latest version contains a new adaptation scheme together with a more efficient multi-point mating procedure.

This research plan result was developed within MSM0001066901 institutional research plan  "External aerodynamics development (2004-2010, MSM)" provider MŠMT.

software

user manual

Crack-XFEM

Program Crack-XFEM is XFEM (extended finite element method) implementation within MATLAB for modelling plane stress and plane strain crack growth and calculation stress intesity factor of edge crack and center crack. XFEM together with Level set method enable crack growth modelling without the need of grid remeshing. Paris Law is used for crack growth. Inclusion and void can be included into geometry.

This research plan result was developed within MSM0001066903 institutional research plan  "Research of strength of low-weight structures with special regard to airplane structures (2004-2010, MSM)" provider MŠMT.

software

user manual

KORELA 1.0

Software tool for comparison of eigenvectors of the aircraft structures gained either by experimental or by analytical approach by means of the MAC criterion. Program can be used for verification and tuning of the analytical model.

This research plan result was developed within MSM0001066903 institutional research plan  "Research of strength of low-weight structures with special regard to airplane structures (2004-2010, MSM)" provider MŠMT.

software

user manual

A2OSCEU, v. 1.0

Parallel software used for the solution of the 2D inviscid flow in the vicinity of an airfoil. The Euler equations are solved on the structured meshes, numerical solution is based on the finite volume method. For the higher accuracy Van Albada limiter is used. Explicit time marching is used, software computes the given number of iterations.

This research plan result was developed within MSM0001066902 institutional research plan  "Research on the high-speed aerodynamics experimental and numerical methods and tools with respect to enhancement of engineering devices efficiency in the field of aeronautics and power engineering (2004-2010, MSM)" provider MŠMT.

software

user manual (EN version)

A2OSCEARSM, v. 1.0

Parallel software used for the solution of the 2D turbulent flow in vicinity of an airfoil. The RANS equations with the EARSM are solved on structured meshes, numerical solution is based on the finite volume method. For higher accuracy Van Albada limiter is used. Explicit time marching is used, software computes given number of iterations.

This research plan result was developed within MSM0001066902 institutional research plan  "Research on the high-speed aerodynamics experimental and numerical methods and tools with respect to enhancement of engineering devices efficiency in the field of aeronautics and power engineering (2004-2010, MSM)" provider MŠMT.

software

user manual (EN version)

T3KOT, v. 1.0

Software used for the solution of the 3D turbulent flow in the channels, the temperature is preffered at the outlet. The k-w RANS equations are solved on structured meshes, numerical solution is based on finite volume method. For higher accuracy Van Albada limiter is used. Explicit time marching is used, software computes given number of iterations.

This research plan result was developed within MSM0001066902 institutional research plan  "Research on the high-speed aerodynamics experimental and numerical methods and tools with respect to enhancement of engineering devices efficiency in the field of aeronautics and power engineering (2004-2010, MSM)" provider MŠMT.

software

user manual (EN version)

T3KOQ, v. 1.0

Software used for the solution of the 3D turbulent flow in the channels, the mass flow is preffered at the outlet. The k-w RANS equations are solved on structured meshes, numerical solution is based on the finite volume method. For higher accuracy Van Albada limiter is used. Explicit time marching is used, software computes given number of iterations.

This research plan result was developed within MSM0001066902 institutional research plan  "Research on the high-speed aerodynamics experimental and numerical methods and tools with respect to enhancement of engineering devices efficiency in the field of aeronautics and power engineering (2004-2010, MSM)" provider MŠMT.

software

user manual (EN version)

T3EARSMQ, v. 1.0

Software used for the solution of the 3D turbulent flow in the channels, the mass flow is preffered at the outlet. The RANS equations with the EARSM are solved on structured meshes, numerical solution is based on the finite volume method. For higher accuracy Van Albada limiter is used. Explicit time marching is used, software computes given number of iterations.

This research plan result was developed within MSM0001066902 institutional research plan  "Research on the high-speed aerodynamics experimental and numerical methods and tools with respect to enhancement of engineering devices efficiency in the field of aeronautics and power engineering (2004-2010, MSM)" provider MŠMT.

software

user manual (EN version)

T3EARSMT, v. 1.0

Software used for the solution of the 3D turbulent flow in the channels, the temperature is preffered at the outlet. The RANS equations with EARSM are solved on structured meshes, numerical solution is based on the finite volume method. For higher accuracy Van Albada limiter is used. Explicit time marching is used, software computes given number of iterations.

This research plan result was developed within MSM0001066902 institutional research plan  "Research on the high-speed aerodynamics experimental and numerical methods and tools with respect to enhancement of engineering devices efficiency in the field of aeronautics and power engineering (2004-2010, MSM)" provider MŠMT.

software

user manual (EN version)

C2DUM, v. 1.0

Parallel software used for the solution of the 2D compressible flow. The Euler equations, the Navier Stokes equations, or the RANS with the k-w or EARSM turbulent model are solved on the unstructured meshes (triangular, quadrilateral), numerical solution is based on the finite volume method. To achieve the higher accuracy Van Albada and Barth-Jespersen limiters are used. THe explicit time marching is used.

This research plan result was developed within MSM0001066902 institutional research plan  "Research on the high-speed aerodynamics experimental and numerical methods and tools with respect to enhancement of engineering devices efficiency in the field of aeronautics and power engineering (2004-2010, MSM)" provider MŠMT.

software

user manual (EN version)

StabCont

Application for computation of nonlinear motion of aircraft and flying qualities.

This research plan result was developed within MSM0001066901 institutional research plan  "External aerodynamics development (2004-2010, MSM)" provider MŠMT.

software

user manual

@EROiDENT 1.2

Application for the identification of flight parameters using the maximum likelihood method.

This research plan result was developed within MSM0001066901 institutional research plan  "External aerodynamics development (2004-2010, MSM)" provider MŠMT.

software

user manual

View JPG

Program for Labview 8.5 for reading and viewing JPG file, converting it to digital data and sending it back for further processing.

This research plan result was developed within MSM0001066902 institutional research plan  "Research on the high-speed aerodynamics experimental and numerical methods and tools with respect to enhancement of engineering devices efficiency in the field of aeronautics and power engineering (2004-2010, MSM)" provider MŠMT.

software

user manual

PIV-AV

Program PIV-AV enables postprocessing PIV measurement data. It offers visualisation and exports velocity field, vorticity field, streamlines and velocity field arrow plot. Program enables export of each shot for video creation, and statistical analysis of the whole record. It also enables point and line analysis. Because of the need to cover shaded area, user is able to define it, and it can be covered by a static picture.

This research plan result was developed within MSM0001066901 institutional research plan  "External aerodynamics development (2004-2010, MSM)" provider MŠMT.

software

user manual

CpInt3D

Program enables calculation of lift coefficient and side force coefficient from 3D pressure coefficient distribution, acquired from CFD calculation. Nodes separation for upper and lower surface, needed for calculation of pressure coefficient difference, can be done by loading a separation surface, or can be estimated in program directly. Program enables transfer of results on set up 2D grid, or direct set of slices by user.

This research plan result was developed within MSM0001066901 institutional research plan  "External aerodynamics development (2004-2010, MSM)" provider MŠMT.

software

user manual

AcBuilder

AcBuilder is a software intended for aircraft conceptual design. It allows creating of parametrized geometry of aircraft including interactive 3D visualization, entering input parameters for modules of CEASIOM software and calculation of basic geometrical and weight quantities.

This research plan result was developed within MSM0001066901 institutional research plan  "External aerodynamics development (2004-2010, MSM)" provider MŠMT.

software (for win32)

User manual (EN version)

Program for selection and signal conditioning

The software for selection and signal conditioning is used to retrieve the input signal and its treatment by filtering according to the specified parameters.

This research plan result was developed within MSM0001066901 institutional research plan  "External aerodynamics development (2004-2010, MSM)" provider MŠMT.

software

user manual

Software for displaying and comparison of charts

Program for viewing and comparison of charts is used to retrieve measured results from the files, view and print the charts.

This research plan result was developed within MSM0001066901 institutional research plan  "External aerodynamics development (2004-2010, MSM)" provider MŠMT.

software

user manual

FFT

Program for visual selection, analysis (by the Fast Fourier Transformation) filtering and saving of measured data.

software

user manual

MakeCalFiles

Program which creates special calibration files with pressure coefficients Cp from calibration of five-tube pressure probe.

This research plan result was developed within MSM0001066901 institutional research plan  "External aerodynamics development (2004-2010, MSM)" provider MŠMT.

software

user manual

VypocetS1

Program for evaluation of air speed and air direction from pressures on the output of five-tube pressure probe. This evaluation is done by the tables of pressure coefficients obtained during calibration of this probe.

This research plan result was developed within MSM0001066901 institutional research plan  "External aerodynamics development (2004-2010, MSM)" provider MŠMT.

software

user manual

McL-calc

Program McL-calc enables postprocessing pressure distribution measurement on airfoil and calculation of lift coefficient with angle of attack correction. Program also offers a possibilty of interpolation of pressure distribution for set angle of attack.

This research plan result was developed within MSM0001066901 institutional research plan  "External aerodynamics development (2004-2010, MSM)" provider MŠMT.

software

user manual

Wind Tunnel

Computational application for design of the closed circuit wind tunnel by the help of quazi-empiric method.

software

user manual

Cfdmsh

Light and open Python Library for CFD hybrid meshing using the Salome Platform GUI (Graphical User Interface), especially around 2D foils. Cfdmsh provides also group and mesh configuration management functions making Salome more flexible regardless the geometry to create and/or to mesh.

software

user manual

Cfdmsh 2.2

Improved version of the previous cfdmsh 1.0 script with numerous new geometrical functions and arguments, accelerated and enhanced group management, as well as improved ergonomics. Cfdmsh 2.2 provides also some 3D functions.

software

manual

Cfdmsh 3.0

Cfdmsh 3.0 provides fourteen new functions and substantial improvements: direct selection of source objects in the Salome's graphical interface and improvement of existing functions. New functions deal with the reconstruction of imported geometries, the import/export of mesh hypotheses, the possibility to define arbitrary refinement areas for Netgen, among others.

sofware

MFAT

Software evaluates the material fatigue life to obtain the influence of maximum stress on the number of cycles to failure.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software

user manual

PODHM

Software evaluates results of a non-destructive detection to obtain the hit/miss model.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software

user manual 

DYNMER

Software useful for control of the National Instruments DAQ cards of the MX family. The software allows visualization and record of mesured dynamic signal. It is possible to visualize the signal in its time and frequency domain.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software

user manual 

Modulus SD_v1

The SD_v1 Modulus is used for signal evaluation as a bandpass filter type which provides information about the amplitude of the filtered harmonic signal and also about its phase. The filter has much better selectivity compared to the commonly used digital approximation filters.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software

user manual

PG1

Program PG1 is primary intended to acquire connectivity of aligning points of 2D slice of 3D mesh. Generally it is a non-convex hull extraction from point data set. There is no unique solution, program offers solution by geometric approach or Dijsktra's algorithm applied to travelling salesman problem. Program run in Matlab.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software user manual

Calcwing1

Calcwing1 is a software intended for calculation of loading of slender elastic wings.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software user manual

SHAVE1

A software solves parameters of shock waves in humid air up to a saturation limit. A special attention was given to solving this case in real conditions of a transonic wind tunnel with an athmospheric intake. The software solves either normal or oblique shocks.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software user manual

Param_TL

This is a software for parametrization of a turbine blade profile based on the Škoda AP1 method. The software can be used to convert a point representation of a blade profile to the set of parameters or to assign geometrical points to the given parameters. The use of the software is mainly in optimization problems.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software user manual

CamView

This program is used to display the image, store pictures and store video from IP cameras Arecont Vision AV5100.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software user manual

AFDB

Software AFDB contains database of 1800 airfoils a their aerodynamic characteristic computed in Xfoil program.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software user manual

bresRead

Software for data reading from *.bres file (binary residual) file, which is saved in FFA-format

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software user manual

MatPlot

Software for displaying of computational mesh and result of CFD in FFA format.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software user manual

tabCL

Software for results displaying of high lift mechanization CFD computation.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software user manual

WTM

Software that processes aerodynamic characteristics from wind tunnel measurement.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software user manual

triMat

Program creates a computational mesh that contains triangular elements.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software user manual

OPTPROFIL version 2012

Software package OPTPROFIL is a universal optimizer of airfoils consisting of the airfoil-evaluation package, airfoil-parameterization package, and a mutli-objective evolutionary algorithm.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software user manual

MIARMOGA version 2012

New better subprograms were implemented in package MIARMOGA, which is a multi-objective micro-genetic algorithm with automatic range-adaptation.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software user manual

C3DRANSKWI

We work with the system of equations describing non-stationary inviscid compressible fluid flow in 3D, i.e. the Renolds-Averaged Navier-Stokes (RANS) equations, and we focus on the numerical solution of these equations and on the boundary conditions. In particular, we choose the implicit finite volume method, and the two-equation turbulent model $k-w$ (Kok), see \cite{Kok}. We use the analysis of the Riemann problem for the construction of the boundary conditions in order to match the experimental data. As a part of this work we present own-developed software for the solution of the 3D RANS equations, using the shown implicit method.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software user manual

C3DNSI

We work with the system of equations describing non-stationary inviscid compressible fluid flow in 3D, i.e. the Navier-Stokes equations, and we focus on the numerical solution of these equations and on the boundary conditions. In particular, we choose the implicit finite volume method. We use the analysis of the Riemann problem for the construction of the boundary conditions in order to match the experimental data. As a part of this work we present own-developed software for the solution of the 3D Navier-Stokes equations, using the shown implicit method.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software user manual

C3DEEI

We work with the system of equations describing non-stationary inviscid compressible fluid flow in 3D, i.e. the Euler equations, and we focus on the numerical solution of these equations and on the boundary conditions. In particular, we choose the implicit finite volume method. Many boundary conditions (i.e. fixed, linearized) bring non-physical errors into the solution, slowing down the convergent process, or even ruining the solution in the whole domain. We use the analysis of the Riemann problem for the construction of the boundary conditions in order to match the experimental data. We show, that the unknown one-side initial condition for the local Riemann problem can be partially replaced by the suitable complementary condition. We suggest such complementary conditions (by preference of pressure, velocity, total quantities,...) giving physically relevant data. Our method for the construction of the boundary conditions is robust and its use accelerates the solver convergence to the desired solution. As a part of this work we present own-developed software for the solution of the 3D Euler equations, using the implicit method.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software user manual

AFKOV

The software pack AFKOV can be used for the solution of the Reynolds-Averaged Navier-Stokes equations for the 2D turbulent flow with the k-omega turbulence model. Software is intended to be used for the solution of the viscous turbulent flow through the diffusible barrier.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software user manual

OSTEP

The software pack OSTEP can be used for the solution of the heat equation for the axis-symmetrical body. It uses the finite volume method.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software user manual

D3TEP

The software pack D3TEP can be used for the solution of the heat equation for the three-dimensional body.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software user manual

ODISKV

The software pack ODISKV can be used for the solution of the Reynolds-Averaged Navier-Stokes equations for turbulent flow with the k-omega turbulence model. Software is intended to be used for the solution of the viscous turbulent flow through the propeller disk given by a velocity profile.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software user manual

MODEX Filtry 2012

MODEX Filtry 2012 is application for transition function analysis. Software application is necessary tool for parameter choice in AE event recognition from sampled record.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software user manual

MODEX Clusters 2012

There were developed couple applications for online clustering mechanisms for AE data separation. Applications are capable of easy analytical setup of described clustering mechanisms. Cluster analysis results were demonstrated on AE data measured on CT specimens (fracture toughness).

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software user manual

MODEX FBG 2012

Application MODEX FBG is supposed as data acquisition and evaluation software for FOBG measurements and it is consisted from two independent application. First application do transfer of measure data from measured device to evaluation PC and second visualize measured data in time domain and on simple model visualization. Evaluation application allows Excel export of chosen data.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software user manual

TDCDAQ

Tdcdaq provides means for event time and time interval measurement data acquisition, basic statistical processing and graphical real-time presentation. Modular architecture allows to support different one- or two-channel time-to-digit converter devices, using various communication interfaces. Notable features are 128bit signed time arithmetic and included lightweight graph plotting framework on top of FLTK graphical user interface. Source code is publicly available at: https://github.com/hrobotron/tdcdaq

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software user manual

MRSTsFoam

Multi-regional solver for solution reacting flow problems based on RANS equations.

This project result was developed within the 7E12035 project “Efficient Systems and Propulsion for Small Aircraft (2012-2015, MSM/7E)”  provider MŠMT.

software user manual

AFanalyzer

Outputs of the program are (autoregressive) model frequency characteristic with selected natural frequencies and the list box with computed natural frequencies and their damping ratios for each analyzed signal. The program can also compute absolute acceleration shock response spectrum for measured signal.

This project result was developed within the 7E12035 project “Efficient Systems and Propulsion for Small Aircraft (2012-2015, MSM/7E)”  provider MŠMT.

software user manual

 

RFCalc

Software "RFCalc". Evaluation of cycles of the dynamic loading of structures. The software designated for calculation of characterization of a dynamic loading according to so called Rain-flow methods, concretely the four-point approach was used. Input data is a file containing measured sampled signal in correct data format that is consequently reduced to local extremes – peaks and throughs. Some level of range filter can be chosen to omission of small insignificant cycles. The extraction of the individual cycles characterized by their amplitudes and mean values is the first results of calculation. These two parametres of each cycle are then recorded in a matrix which presents cycle frequencies in given load-time history with accuracy according to select matrix size and boundaries.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software user manual

OSWaves

The software contains equations for calculation of parametres of oblique shock waves like pressure, temperature, density and enthropy. Also calculates these parametres in moist air and shows them in a chart.

This project result was developed within the institutional support of the Ministry of Industry and Trade of the Czech Republic directed to the development of research organizations.

software user manual