Abstract
Various closure conditions of a ventilated cavity enveloping all or part of a high-speed underwater body are introduced, including those involving a propulsion jet. The flow regimes for the latter are described based on Efros-Paryshev theory, which is extended to estimate the efficiency and fundamental limitations of a rocket-type propulsor.
Original language | English (US) |
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Article number | 012156 |
Journal | Journal of Physics: Conference Series |
Volume | 656 |
Issue number | 1 |
DOIs | |
State | Published - Dec 3 2015 |
Event | 9th International Symposium on Cavitation, CAV 2015 - Lausanne, Switzerland Duration: Dec 6 2015 → Dec 10 2015 |
All Science Journal Classification (ASJC) codes
- General Physics and Astronomy