Hydrodynamic Performance Data of Multi-stage Pump-Jet Propulsor

Description

This is a set of raw performance data of multi-stage pump-Jet propulsors. The document “Hydrodynamic Performance.xlsx” provides hydrodynamic performance data for different advance ratios under varying axial parameters. Specifically, it includes rotor thrust, rotor torque, total thrust, total torque, etc.

Institutions

• Northwestern Polytechnical University

  Shaanxi, Xi'an

Categories

Funders

• National Natural Science Foundation of China

  Beijing

  Grant ID: 52575312

Licence