| Title |
Fig. 1. Principal block diagram of the hovercraft lift system: — adjustment parameter of the engine operating mode; g — cyclic fuel delivery; — rotation velocity and torque transmitted from the engine; — rotation velocity and torque of the fan; h — hovercraft lift height; Q — air flow rate; — excessive pressure in the air-cushion; — the hovercraft motion conditions coefficient. |
| Submission |
Mathematical model of the hovercraft lift system |
| Type |
author.submit.suppFile.figureResearchResults |
| Date |
2024-02-08 |
| Digital Object Identifier |
https://doi.org/10.17816/2074-0530-585184-4191552 |