Underwater Glider Propulsion Systems VBS Part 1: VBS Sizing and Glider Performance Analysis
Autor: | Noé Amir Rodríguez-Olivares, Tomas Salgado-Jimenez, Juan Pablo Orozco-Muñiz |
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Rok vydání: | 2020 |
Předmět: |
Buoyancy
Underwater glider Computer science angle of attack underwater gliders Ocean Engineering Propulsion engineering.material 01 natural sciences 010305 fluids & plasmas lcsh:Oceanography lcsh:VM1-989 Range (aeronautics) 0103 physical sciences glider polar chart lcsh:GC1-1581 variable buoyancy system 0105 earth and related environmental sciences Water Science and Technology Civil and Structural Engineering 010505 oceanography Angle of attack Volume (computing) Glider lcsh:Naval architecture. Shipbuilding. Marine engineering specific energy consumption Sizing glider performance engineering Marine engineering |
Zdroj: | Journal of Marine Science and Engineering Volume 8 Issue 11 Journal of Marine Science and Engineering, Vol 8, Iss 919, p 919 (2020) |
ISSN: | 2077-1312 |
DOI: | 10.3390/jmse8110919 |
Popis: | The Variable Buoyancy System (VBS) is a critical device in the operation of underwater gliders that should be properly sized to achieve the required vehicle propulsion safety within the operating range and adequate efficiency at the nominal depth rating. The VBS budget volume depends mainly on the glider hydrodynamics and the main operating states of the vehicle. A method is proposed with analytical equations to analyze the performance of underwater gliders and to estimate the resultant velocities of the vehicle as a function of the buoyancy change and the glider angle. The method is validated to analyze the glider performance of underwater gliders and is essential to get the main design requirement for the propulsion system: the VBS budget volume. The paper presents the application of the method to obtain the VBS sizing for an academic glider a comparison with the historical hydrodynamic data of the Slocum glider the results of the glider performance study and the development of the characteristic charts necessary to evaluate the performance of the vehicle and its flight parameters. |
Databáze: | OpenAIRE |
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