Using Optical Methods to Image Shockwaves in Low-Pressure Areas in Order to Increase Accuracy of Simulations of Gas Flows Within Low-Pressure Areas

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26220%2F17%3APU124937" target="_blank" >RIV/00216305:26220/17:PU124937 - isvavai.cz</a>

Výsledek na webu

<a href="http://dx.doi.org/10.1149/08101.0305ecst" target="_blank" >http://dx.doi.org/10.1149/08101.0305ecst</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.1149/08101.0305ecst" target="_blank" >10.1149/08101.0305ecst</a>

Jazyk výsledku

angličtina

Název v původním jazyce

Using Optical Methods to Image Shockwaves in Low-Pressure Areas in Order to Increase Accuracy of Simulations of Gas Flows Within Low-Pressure Areas

Popis výsledku v původním jazyce

The area of a shockwave is the most specific area of a supersonic gas flow because its general shape is affected not only by the gas itself but also by the pressure difference between the operating (input) pressure and the atmospheric (output) pressure and by the shape of the aperture or jet the gas passes through. Simulating a supersonic gas flow leaving a jet into a high-pressure area requires to use specific constant values depending on the type of the gas and boundary conditions, which were already experimentally verified. However, when simulating a supersonic gas flow entering a low-pressure (or vacuum) area, different constant values are needed. This paper deals with a possibility of using optical methods for displaying a shockwave within a low-pressure area in order to modify a numerical model of the flow to make the simulated shockwave match the one from experiment.

Název v anglickém jazyce

Using Optical Methods to Image Shockwaves in Low-Pressure Areas in Order to Increase Accuracy of Simulations of Gas Flows Within Low-Pressure Areas

Popis výsledku anglicky

The area of a shockwave is the most specific area of a supersonic gas flow because its general shape is affected not only by the gas itself but also by the pressure difference between the operating (input) pressure and the atmospheric (output) pressure and by the shape of the aperture or jet the gas passes through. Simulating a supersonic gas flow leaving a jet into a high-pressure area requires to use specific constant values depending on the type of the gas and boundary conditions, which were already experimentally verified. However, when simulating a supersonic gas flow entering a low-pressure (or vacuum) area, different constant values are needed. This paper deals with a possibility of using optical methods for displaying a shockwave within a low-pressure area in order to modify a numerical model of the flow to make the simulated shockwave match the one from experiment.

Druh

D - Stať ve sborníku

CEP obor

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OECD FORD obor

20201 - Electrical and electronic engineering

Projekt

<a href="/cs/project/LO1210" target="_blank" >LO1210: Energie v podmínkách udržitelného rozvoje (EN-PUR)</a><br>

Návaznosti

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

Rok uplatnění

2017

Kód důvěrnosti údajů

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

Název statě ve sborníku

ECS Transections

ISBN

978-80-214-5384-5

ISSN

1938-5862

e-ISSN

1938-6737

Počet stran výsledku

6

Strana od-do

1-6

Název nakladatele

Neuveden

Místo vydání

Neuveden

Místo konání akce

Antonínská 1, Brno

Datum konání akce

28. 8. 2016

Typ akce podle státní příslušnosti

WRD - Celosvětová akce

Kód UT WoS článku

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