Parametric Study of a Cavitation Valve for Control of Oxidizer Flow in a Hybrid Rocket Engine

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F13%3APU104315" target="_blank" >RIV/00216305:26210/13:PU104315 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Result language
angličtina
Original language name
Parametric Study of a Cavitation Valve for Control of Oxidizer Flow in a Hybrid Rocket Engine
Original language description
Part of a collaborative European effort to advance throttleable hybrid rocket technology, Bradford Engineering is developing a cavitating flow control valve. In order to improve performance of the valve Brno University of Technology has performed extensive numerical simulation campaign resulting in new valve design. The paper describes design considerations of the cavitating valve as well as characterization of the valve performance by experimental and numerical means. Furthermore, numerical parametricstudy is performed together with experimental evaluation of the optimized design.
Czech name
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Czech description
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Project
<a href="/en/project/ED0002%2F01%2F01" target="_blank" >ED0002/01/01: NETME Centre (New Technologies for Mechanical Engineering)</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year
2013
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
21st SVS FEM Ansys Users' Group Meeting and Conference Proceedings 2013
ISBN
978-80-905525-0-0
ISSN
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e-ISSN
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Number of pages
15
Pages from-to
1-15
Publisher name
SVS FEM
Place of publication
Škrochova 3886/42, 615 00, Brno
Event location
Luhačovice
Event date
Jun 12, 2013
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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