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1D Thermodynamical Model of Gas Turbine Engine

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F20%3A00360292" target="_blank" >RIV/68407700:21220/20:00360292 - isvavai.cz</a>

  • Result on the web

    <a href="https://www.fs.cvut.cz/ustavy/sekce-centrum-leteckeho-a-kosmickeho-vyzkumu/centrum-leteckeho-a-kosmickeho-vyzkumu-12203/centrum-12203/" target="_blank" >https://www.fs.cvut.cz/ustavy/sekce-centrum-leteckeho-a-kosmickeho-vyzkumu/centrum-leteckeho-a-kosmickeho-vyzkumu-12203/centrum-12203/</a>

  • DOI - Digital Object Identifier

Alternative languages

  • Result language

    angličtina

  • Original language name

    1D Thermodynamical Model of Gas Turbine Engine

  • Original language description

    Software for calculating the thermodynamic parameters of a turbine aircraft engine based on generally known physical relationships and supplemented with realistically measured characteristics and parameters.

  • Czech name

  • Czech description

Classification

  • Type

    R - Software

  • CEP classification

  • OECD FORD branch

    20304 - Aerospace engineering

Result continuities

  • Project

    <a href="/en/project/EF16_019%2F0000826" target="_blank" >EF16_019/0000826: Center of Advanced Aerospace Technology</a><br>

  • Continuities

    P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Others

  • Publication year

    2020

  • Confidentiality

    S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Data specific for result type

  • Internal product ID

    12203_CASR_Parez_VES1.0

  • Technical parameters

    The calculation tool allows the calculation of thermodynamic parameters of the gas turbine engine.The calculation is divided into substructural nodes which are: inlet system, compressor, combustion chamber, turbine and outlet. The calculation works on the basis of the engine steady states. The input parameters are limited by the international standard atmosphere standards used in the calculation of aircraft engines.

  • Economical parameters

    The software works based on scripts in Matlab. The calculation defines the important thermodynamic parameters of the gas turbine engine in steady state operation. The input is arbitrarily set engine operating parameters and specific characteristics of the design nodes. The use of these output parameters is possible when designing new structures and defining boundary conditions during its development. The economic benefit is possible when used by specific entities involved in power generation, development and research of aircraft engines and gas turbines.

  • Owner IČO

    68407700

  • Owner name

    České vysoké učení technické v Praze / FS / centrum leteckého a kosmického výzkumu