Computational analysis of two-phase flow in a converging-diverging propulsion nozzle suitable for water transport

Author:

Mangela Divyesh B,Raj Arun KORCID,Mohanan K P,Jayaraj S

Publisher

Springer Science and Business Media LLC

Subject

Multidisciplinary

Reference29 articles.

1. Mottard E J and Shoemaker C J 1961 Preliminary investigation of an underwater ramjet powered by compressed air. National Aeronautics and Space Administration. https://apps.dtic.mil/sti/citations/AD0268736

2. Muir J F and Eichhorn R 1963 Project SQUID: Compressible Flow of an Air-Water Mixture through a Vertical, Two-Dimensional, Converging-Diverging Nozzle. Princeton Univ Nj Dept of Mechanical and Aerospace Engineering. https://ntrl.ntis.gov/NTRL/dashboard/searchResults/titleDetail/ADA952466.xhtml

3. Witte J H 1969 Predicted performance of large water ramjets. AIAA paper. In: Proceedings of the 2nd Advanced Marine vehicles and propulsion Meeting. Washington, USA: American Institute of Aeronautics and Astornautics Inc., 3-47

4. Pierson J D 1965 An application of hydropneumatic propulsion to hydrofoil craft. J. Aircraft 2(3): 250–254. https://doi.org/10.2514/3.43647

5. Schell J, Charles Jr, Harold O, Martin and Marietta Corp 1960 Hydro-pneumatic ramjet. US Patent 3,171,379. https://patents.google.com/patent/US3171379A/en

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