Numerical study on ignition start-up process of an underwater solid rocket motor across a wide depth range-Reference-Cited by-同舟云学术

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Numerical study on ignition start-up process of an underwater solid rocket motor across a wide depth range

Published:2024-06 Issue: Volume: Page:
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

WANG Deyou,LI Shipeng,JIN Ge,WANG Ruyao,GUAN Dian,WANG Ningfei

Publisher

Elsevier BV

Reference51 articles.

1. Experimental study on ignition process of a magnesium-based water ramjet engine;Huang;J Propuls Power,2014

2. Effect of primary water injection angle on thermal propulsion performance of a water ramjet engine;Liu;Aerosp Sci Technol,2020

3. Unsteadiness of flow separation and end-effects regime in a thrust-optimized contour rocket nozzle;Nguyen;Flow Turbul Combust,2003

4. Numerical investigation of flow separation behavior in an over-expanded annular conical aerospike nozzle;He;Chin J Aeronaut,2015

5. Experimental data from underwater conical nozzles exhausting N2 gas;Ferguson;J Hydronautics,1969

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