Numerical and experimental evaluation of the performance of a cavitating valve for the 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%3APU104336" target="_blank" >RIV/00216305:26210/13:PU104336 - 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
Numerical and experimental evaluation of the performance of a cavitating valve for the 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. The paper describes design considerations of the valve assembly as well as characterization of the valve performance by experimental and numerical means.
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
5th European Conference for Aeronautics and Space Sciences EUCASS 2013 proceedings
ISBN
978-84-941531-0-5
ISSN
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e-ISSN
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Number of pages
9
Pages from-to
1-9
Publisher name
EUCASS
Place of publication
Munich, Germany
Event location
Mnichov
Event date
Jul 1, 2013
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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