Licenced software
If you are interested to get a licenced software, please contact the Projects and Contracts Department.
Licence Agreement (only Czech version available)
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| Name | Annotation | Files to download |
| ACEV 1.0 | Software is intended for visualization, editing and exporting data and graphics of aerodynamic characteristics. Program allows user to smooth data using polynomial fitting, moving average or local linear regression. | User manual (CZ version) |
| CPEI 1.0 | Software for editing and integration of the distribution coefficient of pressure. Allows modification of data containing the coordinates and the values of the coefficient of pressure by adjusting a graphical display and calculation of the coefficient of lift by integrating the distribution coefficient of pressure. | User manual (CZ version) |
| A2KO 1.0 | Parallel software used for the solution of the 2D turbulent flow in vicinity of an airfoil. Standard 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. | User manual (EN version) |
| A2OSCKO 1.0 | Software solutions for 3D Navier-Stokes equations for turbulent flow with (k, w) modified turbulence model. | User manual (EN version) |
| T3KO 1.0 | SW used for the solution of the viscous turbulent flow through the 3D channels, structured mesh consisting of four walls, two of them are parallel, one inlet boundary, one outlet boundary. | User manual (EN version) |
| TAS3KO 1.0 | SW used for the solution of the viscous turbulent flow through the 3D channels, structured mesh consisting of four walls, two of them are parallel, one inlet boundary, one outlet boundary. | User manual (EN version) |
| T3EARSM 1.0 | SW for the solution of the viscous turbulent flow through the anulus-shaped 3D channels. Inner cylinder wall may rotate at given angular velicity. | User manual (EN version) |
| INSTEJ 1.0 | Numerical method for computation of a flow field in a 2D supersonic ejector. | User manual (EN version) |
| INST3D 1.0 | Development of a numerical code for a solution of a 3D turbulent flow described by an EARSM model. | User manual (EN version) |
| DPR Calc Kd | Programs serve for calculation Kd (constant of mechanical damping Kd [N.m.s.rad-1] ) from measured file. The result is saved to questionnaire file. | User manual (EN version) |
| DPR Calc Inertia | Programs serve to calculation moment of Inertia [kg*m2] from measured file. The model inertia moments depends on ks spring constant and frequency of oscillation. The result is saved to questionnaire file. | User manual (EN version) |
| DPR Calc Derivative | Programs serve for calculation aeroidynamic Derivatives any given aircraft from measured file. It is used for oscilations in pitch, yaw and roll. The results are saved to result file. | User manual (EN version) |
| VAISALA | Application for reading, saving and presentation of data from vaisala PTU200. Vaisala PTU200 is unit to measure barometric pressure, temperature and humidity. Application read this values by RS485 in set interval and save it into a file and present it in a graph. | User manual (CZ version) |
| URANS2DMBI | Software solves unsteady 2D compressible viscous turbulent flow in a stator-rotor system. | User manual (CZ version) |
| PROPFM 1.0 | Software tool for calculation of the propeller aerodynamic matrices (formally stiffness and damping matrices) for the whirl flutter analysis. Program prepares the input data for the analysis by means of the FE NASTRAN system. | Description of the functionality of the program is subject to trade secrets and may be conditionally made available on request. |
| KALSNIM 2.0 | Accelerometer calibration is adjusting the charge amplifier sensitivity so that the measured acceleration is the same as the etalon value. | User manual (CZ version) |
| KALVIBR 3.0 | Exciter calibration is determining of exciter constant connecting in exciting loop. The method is established on the acceleration change measurement of a basic vibration system when the accurate mass is added. | Description of the functionality of the program is subject to trade secrets and may be conditionally made available on request. |
| OPTIMEX 2.0 | Calculation of all combination of force vectors from candidate points from one to choose force point number. Result evaluation according to proposed criterion function. Excitation vector contains exciters location and forces amplitude. | Description of the functionality of the program is subject to trade secrets and may be conditionally made available on request. |
| ANALYZ 1.0.0 | Software tool for the graphic processing of the numerical ASCII files. | User manual (CZ version) |
| FINDFLUT 2.1.2 | Software tool for the calculation of the flutter speed and automatic graphic postprocessing of the flutter analysis results, performed by the FE NASTRAN system (V-g-f plot). | User manual (CZ version) |
| PGAOS 1:6 | SW for the aerodynamic optimization of propeller geometry The software is composed from the six computer codes. | User manual (CZ version) |
| EMIARMOGA v.2009 | Microgenetic multicriteria algorithm for solving optimization problems such as aerodynamic profiles, strain-gauge scales and wings of aircraft. | User manual (CZ version) |
| EROiDENT 1.1 | Application for the identification of flight parameters using the method of least squares. | User manual (CZ version) |
