Study of pressure surge during priming phase of start transient in an initially unprimed pump-fed liquid rocket engine-Reference-Cited by-同舟云学术

Study of pressure surge during priming phase of start transient in an initially unprimed pump-fed liquid rocket engine

Published:2022-09 Issue:3 Volume:11 Page:353-375
ISSN:2212-540X
Container-title:Propulsion and Power Research
language:en
Short-container-title:Propulsion and Power Research

Author:

Das Debanjan,Padmanabhan P.

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Fuel Technology,Aerospace Engineering,Automotive Engineering

Reference31 articles.

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2. Development and application of a priming surge analysis methodology;Hearn,2005

3. Numerical modeling of fluid transients by a finite volume procedure for rocket propulsion systems;Majumdar,2003

4. Advanced liquid rocket engine transient model;Ruth,1990

5. An RL10A-3-3A Rocket Engine Model Using the Rocket Engine Transient Simulator (ROCETS) Software, Contractor Report, July, 1993, NASA CR-190786.;Binder,1993

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