An investigation of a cavitating venturi flow control feature in a cryogenic propellant delivery system

Author:

Mena José Luis,Ingle Marjorie A.,Shirsat Vivek,Choudhuri Ahsan

Funder

NASA

Publisher

Elsevier BV

Subject

Electrical and Electronic Engineering,Computer Science Applications,Instrumentation,Modeling and Simulation

Reference10 articles.

1. Hunzel, DK and Huang, DH.. Design of liquid propellant rocket engines. Scientific and technical Infomration Division, Office of Technology, National Aeronautics and Space Administration, 1967.

2. Rocket propulsion elements;Sutton,2001

3. Schmidt, DP and Corradini, ML. One-dimensional analysis of cavitating orifices. Informally published manuscript, Engine Research Center, University of Wisconsin. Downloaded in August 2013, (〈http://thehuwaldtfamily.org/jtrl/research/Hydrodynamics/1D Analysis of Cavitating Orifices.pdf〉).

4. Application of small size cavitating venturi as flow controller and flow meter;Ghassemi;Flow Meas Instrum,2011

5. Majumdar, A. Numerical modeling of cavitating venturi – a flow control element of propulsion system. NASA Marshall Space Flight Center, Theromodynamic and Heat Transfer Group, (〈http://tfaws.nasa.gov/TFAWS02/Data/Propulsion/Majumdar.pdf〉); 2002.

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