Software for numerical solution of flow through 2D blade cascades, v 2.0
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F16%3A00304238" target="_blank" >RIV/68407700:21220/16:00304238 - isvavai.cz</a>
Result on the web
<a href="http://mat.fs.cvut.cz/asw" target="_blank" >http://mat.fs.cvut.cz/asw</a>
DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
Software for numerical solution of flow through 2D blade cascades, v 2.0
Original language description
The software, version 2.0, can be used for two different configurations of blade cascade. The periodical case with infinite number of identical profiles is solved in the domain of one pitch. The second configuration is the model of 2D wind tunnel cross section (transonic wind tunnel of IT CAS) with finite cascade of profiles mounted inside test section. Also the 2.0 version of in house software solves the system of Reynolds Averaged Navier-Stokes (RANS) equations and two equation turbulence model on structured multi-block grid. The steady flow is computed by originally implemented higher order implicit finite volume method with AUSM type scheme for convective terms and common central approximation of dissipative terms. The computational code is complemented by post processing tools, which allows evaluation of proper aerodynamics characteristics of computed flow through cascade. Many parameters of mathematical model and numerical algorithm have been tested and results were compared with experimental data in the period 2014 – 2016. The 2.0 software version contains improvements based on the achieved experiences. It increases applicability of software for complicated cases, even though small deficiencies were observed in computed results for some geometries and flow regimes. The software has been tested for transonic flow in wind tunnel test section with mounted tip section type turbine cascade and transonic flow through infinite profile cascade with supersonic inlet flow. The software is the computational kernel (Linux), which performs the numerical simulation. The software is available in a form of paid license. The potential user has to succeed in a several days training course at the workplace of software owner. The contact person: secretary of the Department of Technical Mathematics, Faculty of Mechanical Eng., TU Prague.
Czech name
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Czech description
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Classification
Type
R - Software
CEP classification
BK - Liquid mechanics
OECD FORD branch
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Result continuities
Project
<a href="/en/project/TA03020277" target="_blank" >TA03020277: Aerodynamics of Highly Loaded Blade Cascades</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Others
Publication year
2016
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Internal product ID
ASW_16_1
Technical parameters
Computing code for Linux. The potential user have to succed in a several days individual training course at the workplace of software owner.
Economical parameters
The software is available in a form of paid license. The software can increase efficiency of wind tunnel experiments and transfer of experimental data into blade design.
Owner IČO
68407700
Owner name
Fakulta strojní