JBoss, an open source application server, by default is configured with the Hypersonic database. JBoss是一个开源应用服务器,在默认情况下,使用Hypersonic数据库来配置它。
A novel nonlinear adaptive control method is presented for a near-space hypersonic vehicle ( NHV) in the presence of strong uncertainties and disturbances. 针对存在强烈不确定和干扰的近空间高超声速飞行器(NHV),提出了一种新的非线性自适应控制方法。
Research on the Liquid-Solid Coupling Dynamics in a Cylindrical Container in the Hypersonic Vehicle 高超声速飞行器中圆柱类贮箱液固耦合动力学研究
Simulation studies show this method is feasible to longitudinal model of hypersonic vehicle. 仿真研究表明,应用该方法来研究高超声速飞行器纵向模型是可行的。
The thermal environment of the wedge leading edge is rigorous in hypersonic flow. 高超声速气流条件下,尖楔前缘的热环境非常恶劣。
Design of Variable Structure Control System for Hypersonic BTT Vehicle 高超音速BTT巡航飞行器变结构控制系统设计
Turbulence modeling validation in hypersonic complex flows 高超声速复杂流动中湍流模式应用的评估
The essential of using experimental design method to configuration design of hypersonic aircraft are expounded. 阐述了在进行高超声速飞行器外形设计中,应用试验设计方法的必要性。
Numerical Study of Pitching Dynamic Characteristic for Hypersonic Missile 高超声速弹头俯仰动态特性数值研究
Aerodynamic Heating and Electron Distribution Research on Hypersonic Warhead 高超声速弹头气动热及电子分布的研究
Experimental study of flow characteristics and the influence for a hypersonic flight vehicle 高超声速飞行器内流道流态及其对全机气动力影响的实验研究
Departures form the ideal practice followed by the Wright have been particularly noticeable in the development of supersonic and hypersonic vehicles. 特别值得注意的是在发展超音速和高超音速飞行器的过程中,偏离了莱特理想的工作方式。
Research on Analysis of Thermal Environment and Structure of Nose Tip for Hypersonic Vehicle 高超声速飞行器鼻锥的热环境和结构热分析研究
A new method of quickly generating hypersonic waverider forebody configurations was developed. 发展了一种基于分析法的高超声速乘波构型飞行器前体设计方法。
Experimental Study on Hypersonic Aerodynamic Characteristics of Aerospace Plane Configuration 一种空天飞机外形高超声速气动特性实验研究
A study is carried out on a hypersonic inlet with rectangular-to-circular shape transition and forebody using numerical simulation and high enthalpy wind tunnel test. 对一种带前体的高超声速矩转圆形进气道开展了数值仿真及高焓脉冲风洞试验研究。
This paper presents the separation shock motion features induced by a hemicylindrically blunted fin in a hypersonic turbulent flow. 给出半圆柱前缘舵诱导的高超声速湍流分离激波运动特性。
Numerical Study of Attack Angle Characteristics for Integrated Hypersonic Vehicle 一体化高超声速飞行器攻角特性的数值研究
In this paper the results of calculations of the coefficients of skin friction and heat transfer ( Stanton number) on the surface of hypersonic flight vehicle are presented. 本文给出了高超声速飞行器表面摩阻和传热系数(斯坦顿数)的计算结果。
A method using CFD technology is used for accurate prediction of aerodynamic force and heat of air-breathing hypersonic vehicles. 对吸气式高超声速飞行器而言,物面热流和摩阻的准确预测对飞行器设计及安全十分关键。
A conceptual design of the hypersonic civil transport is introduced here. 介绍了高超声速民用运输机的概念设计方案。
This formulation can ensure the longitudinal flight stability and improve the control performance of hypersonic vehicles. 该控制方案保证了飞行的纵向稳定性,改善了其控制性能。
Military requirements of hypersonic vehicle and the classification of plasma drag reduction are analyzed briefly. 简单概述了高超声速飞行器的军事需求及等离子体减阻技术的分类;
Study of Optimization Method for Two-Dimensional Hypersonic Inlet 二维高超声速进气道优化设计方法研究
Aerodynamic Heating and Thermal Stress Analysis of ZrB_2-SiC and C/ C Composites in Hypersonic Flows ZrB2-SiC和C/C复合材料高超声速气动加热与热应力分析
Through ground test and hypersonic flow research, he made great progress in air-breathing hypersonic technology. 通过地面试验和高超声速非平衡流的研究,取得了再入突防气动物理的重要进展。
Advised on hypersonic activities for other divisions, the High Speed Civil Transport, sonic boom, ozone environment, and rocket SSTO concepts. 建议对其他部门,高速民用运输,爆音,臭氧环境,和火箭的单级入轨概念的超音速活动。
The account, privilege and audit information is stored in an embedded Hypersonic database. 帐号、权限和审计信息存储于一个嵌入式Hypersonic数据库中。
Hypersonic viscous interaction effects on measurement of free stream pressure in test section are studied through theoretical analysis, experiment measurement and numerical simulation. 通过理论分析、验测量和数值模拟,研究高超声速粘性相互作用对实验段自由流静压测量的影响。