Detail publikace

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

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

Jazyk

en

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.

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",
  annote="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.",
  address="EUCASS",
  booktitle="5th European Conference for Aeronautics and Space Sciences EUCASS 2013 proceedings",
  chapter="100606",
  howpublished="electronic, physical medium",
  institution="EUCASS",
  year="2013",
  month="june",
  pages="1--9",
  publisher="EUCASS",
  type="conference paper"
}