Concepts NREC 126.96.36.199 Suite x86 x64 [2016, ENG]
Size: 615.6 MB Type: Software
Year / Release Date: 2016
AxCent 188.8.131.52 32-bit
AxCent 184.108.40.206 64-bit
Axial 220.127.116.11 32-bit
CADTranslator 8.0.6 32-bit
CADTranslator 8.0.6 64-bit
Compal 18.104.22.168 32-bit
CTAADS 22.214.171.124 32-bit
Fanpal 126.96.36.199 32-bit
Pumpal 188.8.131.52 32-bit
Rital 184.108.40.206 32-bit
Turbomatch 220.127.116.11 32-bit
Turboopti II 18.104.22.168 32-bit
Developer: Concepts ETI, Inc.
All possible crash when selecting some options in programs related to the bugs of the program!
Bit depth: 32bit, 64bit
Medicine: Present (Team-SolidSQUAD)
System requirements: ShiChuang
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.
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
Estimated program preliminary design of axial compressors and turbines
Program zagruzzki and preparation of 3D-models
Estimated program preliminary design of centrifugal compressors and diagonal
The software package for the design of cooled gas turbine blades
Estimated program preliminary design of centrifugal and axial fans
Estimated program preliminary design of centrifugal and axial pumps
Estimated program preliminary design of radial and diagonal turbines
Estimated program for the design of turbochargers
Estimated program for formulating and solving problems of optimization of turbomachinery design