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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.

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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.

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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.

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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.

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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.

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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.

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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.

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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.

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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.

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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.

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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.

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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.

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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.

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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.

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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.

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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.

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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.

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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.

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 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.

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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.

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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.

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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.

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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.

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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.

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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.

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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.

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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.

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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.

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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.

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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.

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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.

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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.

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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.

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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.

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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.

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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

Wingload2 v.2

Wingload2 program is designed to calculate the aerodynamic loads of flexible slender wings of the aircraft, which may be deformed around an elastic torsion axis (not bending). The individual wings are composed of trapezoids with defined 2-dimensional viscous or inviscid profile characteristics at the interfaces of these trapezoids, the elastic axis and the weight distribution. The aerodynamics of the wing is designed NLWing2 program, which is a method of non-linear lifting line. The program outputs are the aerodynamic characteristics of wings and a description of deformation.

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

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

(CZ version)

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.

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