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基于Matlab/Simulink的新型火箭建模与仿真平台搭建 被引量:1
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作者 刘曌 周春华 邱伟 《系统仿真技术》 2018年第4期285-291,共7页
基于火箭建模理论,结合某型火箭数据,建立了Matlab/Simulink环境下的新型箭体模型,并对建立的箭体模型进行仿真验证。将箭体模型按物理意义划分为动力学模型、推力模型、质量模型、重力模型和气动力模型,在Windows操作系统及Lab View_R... 基于火箭建模理论,结合某型火箭数据,建立了Matlab/Simulink环境下的新型箭体模型,并对建立的箭体模型进行仿真验证。将箭体模型按物理意义划分为动力学模型、推力模型、质量模型、重力模型和气动力模型,在Windows操作系统及Lab View_RT实时系统环境下,分别进行模块仿真验证,形成了通用箭体仿真模块库。以搭建的箭体模型为基础,开发了基于Veristand/Lab View_RT半实物仿真平台。型号实测数据对比结果表明:搭建的新型箭体模型正确且有效,可为多型号火箭提供通用箭体仿真模块库。 展开更多
关键词 箭体模型 Matlab建模 半实物仿真 仿真平台
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Geometric effects of fuel regression rate in hybrid rocket motors
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作者 CAI GuoBiao ZHANG YuanJun +3 位作者 WANG PengFei HUI Tian ZHAO Sheng YU NanJia 《Science China(Technological Sciences)》 SCIE EI CAS CSCD 2016年第5期807-813,共7页
The geometric configuration of the solid fuel is a key parameter affecting the fuel regression rate in hybrid rocket motors. In this paper, a semi-empirical regression rate model is developed to investigate the geomet... The geometric configuration of the solid fuel is a key parameter affecting the fuel regression rate in hybrid rocket motors. In this paper, a semi-empirical regression rate model is developed to investigate the geometric effect on the fuel regression rate by incorporating the hydraulic diameter into the classical model. The semi-empirical model indicates that the fuel regression rate decreases with increasing hydraulic diameter and is proportional to dh?0.2 when convective heat transfer is dominant. Then a numerical model considering turbulence, combustion, solid fuel pyrolysis, and a solid–gas coupling model is established to further investigate the geometric effect. Eight motors with different solid fuel grains are simulated, and four methods of scaling the regression rate between different solid fuel grains are compared. The results indicate that the solid fuel regression rates are approximate the same when the hydraulic diameters are equal. The numerical results verify the accuracy of the semi-empirical model. 展开更多
关键词 geometric effect regression rate hydraulic diameter hybrid rocket motor
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