位置：立项数据库 > 立项详情页
空天飞行器高温气体流动研究
  • 项目名称：空天飞行器高温气体流动研究
  • 项目类别：创新研究群体科学基金
  • 批准号：10921062
  • 申请代码：A020404
  • 项目来源：国家自然科学基金
  • 研究期限：2010-01-01-2012-12-31
  • 项目负责人：樊菁
  • 负责人职称：研究员
  • 依托单位：中国科学院力学研究所
  • 批准年度：2009
中文摘要：

中文主题词激波风洞；主动冷却超声速燃烧室；临近空间高超声速飞行；；

中文主题词：
英文摘要：

Shock Tunnel；regenerative cooling for scram；novel hypersonic flight；；

英文主题词： Shock Tunnel；regenerative cooling for scram；novel hypersonic flight；；
成果综合统计
成果类型
数量
  • 期刊论文
  • 会议论文
  • 专利
  • 获奖
  • 著作
  • 84
  • 7
  • 0
  • 0
  • 0
期刊论文
支杆-钝头体带攻角流场和“军刺”挡板作用研究
离心力和滑翔距离对于高超声速巡航飞行性能的影响
Effect of humidity on microstructure and properties of YBCO films prepared by Electron Beam Coevapor
一种新的远程超低巡航飞行方式
超临界压力下航空煤油水平管内对流换热特性数值研究
电子束蒸发制备YBCO超导薄膜研究
Effect of Nozzle Temperature on the Performance of a 1 kW H-2-N-2 Arcjet Thruster
超临界压力下航空煤油流动与传热特性试验
Laser induced breakdown spectroscopy for local equivalence ratio measurement of kerosene/air mixture
冲击射流结构中应用粗糙表面的实验研究
探索发展激波风洞爆轰驱动技术
变比热真实气体效应的高超声速槽道湍流直接数值模拟
Thermal Cracking and Heat Sink Capacity of Aviation Kerosene Under Supercritical Conditions
Aerodynamics of indirect thrust measurement by the impulse method
建设高温气体动力学国家重点实验室支撑我国高超声速科技发展
低功率电弧加热发动机喷管扩张段内壁面温度测量
Underexpanded Supersonic Plasma Jet Generated by a Small Arc-Heated Facility
Numerical research on the complicated structures on the oblique detonation wave surface
Unsteadiness in non-transferred dc arc plasma generators
超临界压力下航空煤油圆管流动和传热的数值研究
高超声速巡航飞行性能的优化分析
Calculation of Hugoniot properties for shocked nitromethane based on the improved Tsien';s EOS
Convective heat transfer characteristics of China RP-3 aviation kerosene at supercritical pressure
Arcjet Thruster Operated With Different Propellants
推进剂组分对电弧加热推力器性能的影响
Study of turbulent heat transfer of aviation kerosene flows in a curved pipe at supercritical pressu
高温壁面热流与温度一体化测量传感器研究
Investigating into techniques for extending the test-duration of detonation-driven shock tunnels
Development of integrated high temperature sensor for simultaneous measurement of wall heat flux and
三面压缩高超进气道附面层抽吸研究
The effect of compressibility on the stability of wall-bounded Kolmogorov flow
Analytical and numerical investigations of the reflection of asymmetric nonstationary shock waves
大内收缩比二元高超声速进气道波系配置特性
超声速气流中煤油射流的等离子体点火实验
Solid wall effect on the transport coefficients of gases
Uncertainty in velocity measurement based on diode-laser absorption in nonuniform flows
气相规则胞格爆轰波起爆与传播统一框架的几个关键基础问题研究
A Compact Sensor Based on Near Infrared Absorption Spectroscopy for Flow Diagnostics in a Low Densit
Measurements of non-equilibrium and equilibrium temperature behind a strong shock wave in simulated
Numerical investigation on unsteady shock wave reflections over three dimensional intersecting wedge
Growth and properties of Cu thin film deposited on Si(001) substrate: A molecular dynamics simulatio
气相爆轰物理的若干研究进展
Mechanisms for non-ideal flow in low-power arc-heated supersonic nozzles
Effect of Nozzle Temperature on the Performance of a 1 kW H2-N2 Arcjet Thruster
高雷诺数方腔流动的分子模拟
Optimal speed of hypersonic cruise flight
Modelling Study to Compare the Flow and Heat Transfer Characteristics of Low-Power Hydrogen, Nitrogen and Argon Arc-Heated Thrusters
预处理气氛对电子束蒸发制备YBCO薄膜性能和结构的影响
会议论文
Molecular Simulation of Small Knudsen Number Flows
Molecular Dynamics Simulation of Deposition and Growth of Cu Thin Film on Si Substrate
Kinetic Studies of Gas Flows
Monte Carlo Simulation of two-dimensional Kolmogorov flow
DEVELOPMENT OF AN EFFICIENT PARTICLE APPROACH FOR MICRO-SCALE GAS FLOW SIMULATIONS
SIMULATION OF GAS FLOW OVER A MICRO CYLINDER
Molecular Motion in Isotropic Turbulence
樊菁的项目
稀薄气体力学
期刊论文 8 专利 3
气固分散体系中连续介质与粒子的耦合方法
“可压缩流动”高级讲习班
空天飞行器高温气体流动研究
期刊论文 82 会议论文 77
微尺度气流的统计模拟
期刊论文 9
气固分散体系中连续介质与粒子的耦合方法