Dynamics Analysis and Testing of Gas-Pressurized Waterjet Rocket

碩士 === 國立中興大學 === 機械工程學系 === 86 === The gas-pressured waterjet rocket makes use of high pressure air as its power source, it can attain high thrust power by consuming less energy. Compared with the traditional rocket, it has more advant...

Full description

Bibliographic Details
Main Authors: Shiah, Wen-Goang, 夏文廣
Other Authors: Lee Hsing-Juin
Format: Others
Language:zh-TW
Published: 1998
Online Access:http://ndltd.ncl.edu.tw/handle/88405434004505713860
Description
Summary:碩士 === 國立中興大學 === 機械工程學系 === 86 === The gas-pressured waterjet rocket makes use of high pressure air as its power source, it can attain high thrust power by consuming less energy. Compared with the traditional rocket, it has more advantages, such as simpler structure, lower cost, better energy efficiency, and etc. Until now, there is no accurate propulsive theory for gas-pressurized waterjet rocket. In order to improve its propulsive efficiency, here we take advantages of Lagrangian Reynolds transport equation, momentum equation, total kinetic power produced by the rocket engine, and propulsion power analysis equations developed by Hsing-Juin Lee. Accordingly, we use computer to simulate and analyze the flight dynamics of gas-pressurized waterjet rocket, thus to aid its design and test for higher altitude. Additionally, this type of gas-pressurized waterjet rocket model includes abundant testing parameters, such as internal flow unsteadiness, acceleration of rocket, gas/water proportion, and etc, to provide versatile applications like analysis, testing and instruction. This type of rocket not only has high education value, but also has the advantages of convenience, safety and environmental protection. Furthermore, because the waterjet rocket has no heat loss, so its propulsive efficiency is the same as its overall efficiency. As the computational result shows that when the propellant (water) absolute velocity approaches zero, its simplified propulsive efficiency is nearly perfect. Herein, we further use generalized propulsive equation to extend the more manipulation space of design parameters. In the future, we may design nozzles with changeable size and curvature to increase its propulsive efficiency. In this paper, we also modify the propulsive efficiency equation to accommodate the situation of the burning out of fuel. Moreover, we may try the design of bursting a small amount of gun-powder to produce high inner pressure to further increase system performance. In addition, we may try the design of a nil-smoke antitank missile, trench mortar, the waterjet rocket carrying life-saving ropes for high-rise building fire accident, or water-shell artillery, and etc.