Research on Two Phase Waterjet Nozzles

Author:

Gowing S.1,Mori T.2,Neely S.1

Affiliation:

1. Carderock Division, Naval Surface Warfare Center, West Bethesda, MD 20817-5700

2. Technical Research and Development Institute, Ministry of Defense, Tokyo 162-8801, Japan

Abstract

Air-augmented waterjets derive their propulsion from compressed gas mixed directly into the main flow. The gas bubbles expand as the mixture passes through the pressure gradient of the convergent nozzle, and energy is imparted to the water from the air in a complex fashion. This experiment measures the exchange of air and water energy for three nozzles over a range of flowrates and void fractions using compressed air injected and mixed upstream of the nozzle entrance. Pressures and nozzle thrust are measured to examine flow changes. The results are compared with predictions from a one-dimensional bubbly flow model. The measured efficiencies are lower than or comparable to predicted values.

Publisher

ASME International

Subject

Mechanical Engineering

Reference19 articles.

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3. Mottard, E. J., and Shoemaker, E. J., 1961, “Preliminary Investigation of an Underwater Ramjet Powered by Compressed Air,” NASA, Report No. TN D-991.

4. An Application of Hydropneumatic Propulsion to Hydrofoil Craft;Pierson;J. Aircr.

5. Design Analysis of Gas-Turbine Powerplants for Two-Phase Hydropropulsion;Pallabazzer

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