Detail publikace

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

DVOŘÁK, P. TIJSTERMAN, R.

Originální název

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

Typ

článek ve sborníku ve WoS nebo Scopus

Jazyk

angličtina

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 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 parametric study is performed together with experimental evaluation of the optimized design.

Klíčová slova

cavitation, control valve, oxidizer, hybrid engine

Autoři

DVOŘÁK, P.; TIJSTERMAN, R.

Rok RIV

2013

Vydáno

12. 6. 2013

Nakladatel

SVS FEM

Místo

Škrochova 3886/42, 615 00, Brno

ISBN

978-80-905525-0-0

Kniha

21st SVS FEM Ansys Users' Group Meeting and Conference Proceedings 2013

Strany od

1

Strany do

15

Strany počet

15

BibTex

@inproceedings{BUT100572,
  author="Petr {Dvořák} and Rob {Tijsterman}",
  title="Parametric Study of a Cavitation Valve for Control of Oxidizer Flow in a Hybrid Rocket Engine",
  booktitle="21st SVS FEM Ansys Users' Group Meeting and Conference Proceedings 2013",
  year="2013",
  pages="1--15",
  publisher="SVS FEM",
  address="Škrochova 3886/42, 615 00, Brno",
  isbn="978-80-905525-0-0"
}