iuly
03-03-2016, 05:18 PM
http://i76.fastpic.ru/big/2016/0303/a3/04638d4c4273944331e58ecaba71cda3.jpg
Year / Release Date: 2016
Version:
AxCent 8.4.11.0 32-bit
AxCent 8.4.11.0 64-bit
Axial 8.4.11.0 32-bit
CADTranslator 8.0.6 32-bit
CADTranslator 8.0.6 64-bit
Compal 8.4.11.0 32-bit
CTAADS 8.4.11.0 32-bit
Fanpal 8.4.11.0 32-bit
Pumpal 8.4.11.0 32-bit
Rital 8.4.11.0 32-bit
Turbomatch 8.4.11.0 32-bit
Turboopti II 8.4.11.0 32-bit
Developer: Concepts ETI, Inc.
ATTENTION!
All possible crash when selecting some options in programs related to the bugs of the program!
Bit depth: 32bit, 64bit *
Language: English
Medicine: Present (Team-SolidSQUAD)
System requirements: Windows
Description: The software package Concepts NREC / Agile Engineering Design System (developer of Concepts ETI, Inc.) provides a single continuous turbomachinery design cycle (compressors, pumps, fans, turbines, turbochargers, expansion machines, etc..), Covering all stages of the design of the one-dimensional, design calculation to manufacture prototype and experimental studies of the process, and solves complex optimization problems.
The software package Concepts NREC includes solvers built on empirical dependencies using the concept of a single or two-band model, the calculation of one-three trickle current solver, based on an analysis of the curvature of the current streams, and so on. E., The Euler equations solution with built-in adjusted for loss, two-dimensional solutions of the problem (two-dimensional Navier-Stokes equations in the inter-blade space height of the flow), as well as solutions 3D CFD viscous tasks and 3D FEA modeling and others.
AxCent
Estimated program for the design of 3D-geometry and calculating the current flow in multistage axial and radial turbomachinery. AxCent features powerful for axial, radial and diagonal geometry, which can be combined to develop almost any turbomachinery
AXIAL
Estimated program preliminary design of axial compressors and turbines
CADTranslator
Program zagruzzki and preparation of 3D-models
COMPAL
Estimated program preliminary design of centrifugal compressors and diagonal
CTAADS
The software package for the design of cooled gas turbine blades
FANPAL
Estimated program preliminary design of centrifugal and axial fans
PUMPAL
Estimated program preliminary design of centrifugal and axial pumps
RITAL
Estimated program preliminary design of radial and diagonal turbines
TURBOMATCH
Estimated program for the design of turbochargers
TurboOPT II
Estimated program for formulating and solving problems of optimization of turbomachinery design
http://i75.fastpic.ru/big/2016/0303/d3/21852382466f938110bb8e9d036653d3.jpg
http://i1221.photobucket.com/albums/dd479/Iulianvis_Iulian/download20100311005411.gif
http://rapidgator.net/file/5428b6d77abd92b32b1d656b76bc80db/Concepts.Nrec.rar.html
http://alfafile.net/file/ReKW/Concepts.Nrec.rar
Year / Release Date: 2016
Version:
AxCent 8.4.11.0 32-bit
AxCent 8.4.11.0 64-bit
Axial 8.4.11.0 32-bit
CADTranslator 8.0.6 32-bit
CADTranslator 8.0.6 64-bit
Compal 8.4.11.0 32-bit
CTAADS 8.4.11.0 32-bit
Fanpal 8.4.11.0 32-bit
Pumpal 8.4.11.0 32-bit
Rital 8.4.11.0 32-bit
Turbomatch 8.4.11.0 32-bit
Turboopti II 8.4.11.0 32-bit
Developer: Concepts ETI, Inc.
ATTENTION!
All possible crash when selecting some options in programs related to the bugs of the program!
Bit depth: 32bit, 64bit *
Language: English
Medicine: Present (Team-SolidSQUAD)
System requirements: Windows
Description: The software package Concepts NREC / Agile Engineering Design System (developer of Concepts ETI, Inc.) provides a single continuous turbomachinery design cycle (compressors, pumps, fans, turbines, turbochargers, expansion machines, etc..), Covering all stages of the design of the one-dimensional, design calculation to manufacture prototype and experimental studies of the process, and solves complex optimization problems.
The software package Concepts NREC includes solvers built on empirical dependencies using the concept of a single or two-band model, the calculation of one-three trickle current solver, based on an analysis of the curvature of the current streams, and so on. E., The Euler equations solution with built-in adjusted for loss, two-dimensional solutions of the problem (two-dimensional Navier-Stokes equations in the inter-blade space height of the flow), as well as solutions 3D CFD viscous tasks and 3D FEA modeling and others.
AxCent
Estimated program for the design of 3D-geometry and calculating the current flow in multistage axial and radial turbomachinery. AxCent features powerful for axial, radial and diagonal geometry, which can be combined to develop almost any turbomachinery
AXIAL
Estimated program preliminary design of axial compressors and turbines
CADTranslator
Program zagruzzki and preparation of 3D-models
COMPAL
Estimated program preliminary design of centrifugal compressors and diagonal
CTAADS
The software package for the design of cooled gas turbine blades
FANPAL
Estimated program preliminary design of centrifugal and axial fans
PUMPAL
Estimated program preliminary design of centrifugal and axial pumps
RITAL
Estimated program preliminary design of radial and diagonal turbines
TURBOMATCH
Estimated program for the design of turbochargers
TurboOPT II
Estimated program for formulating and solving problems of optimization of turbomachinery design
http://i75.fastpic.ru/big/2016/0303/d3/21852382466f938110bb8e9d036653d3.jpg
http://i1221.photobucket.com/albums/dd479/Iulianvis_Iulian/download20100311005411.gif
http://rapidgator.net/file/5428b6d77abd92b32b1d656b76bc80db/Concepts.Nrec.rar.html
http://alfafile.net/file/ReKW/Concepts.Nrec.rar