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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

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

  • Czech description

Classification

  • Type

    R - Software

  • CEP classification

    BK - Liquid mechanics

  • OECD FORD branch

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