Detail publikačního výsledku

Numerical and experimental evaluation of the performance of a cavitating valve for the control of oxidizer flow in a hybrid rocket engine

DVOŘÁK, P.; TIJSTERMAN, R.

Originální název

Numerical and experimental evaluation of the performance of a cavitating valve for the control of oxidizer flow in a hybrid rocket engine

Anglický název

Numerical and experimental evaluation of the performance of a cavitating valve for the control of oxidizer flow in a hybrid rocket engine

Druh

Stať ve sborníku v databázi WoS či Scopus

Originální abstrakt

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.

Anglický abstrakt

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.

Klíčová slova

cavitation, control valve, oxidizer, hybrid engine

Klíčová slova v angličtině

cavitation, control valve, oxidizer, hybrid engine

Autoři

DVOŘÁK, P.; TIJSTERMAN, R.

Rok RIV

2014

Vydáno

30.06.2013

Nakladatel

EUCASS

Místo

Munich, Germany

ISBN

978-84-941531-0-5

Kniha

5th European Conference for Aeronautics and Space Sciences EUCASS 2013 proceedings

Strany od

1

Strany do

9

Strany počet

9

BibTex

@inproceedings{BUT100606,
  author="Petr {Dvořák} and Rob {Tijsterman}",
  title="Numerical and experimental evaluation of the performance of a cavitating valve for the control of oxidizer flow in a hybrid rocket engine",
  booktitle="5th European Conference for Aeronautics and Space Sciences EUCASS 2013 proceedings",
  year="2013",
  pages="1--9",
  publisher="EUCASS",
  address="Munich, Germany",
  isbn="978-84-941531-0-5"
}