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北京航空航天大学 [9]
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Evaluation of the influence of radiation on a GH2/GO2 rocket combustor
会议论文
VIRTUAL EVENT, 2020-08-17
作者:
Li B(李波)
;
Yao W(姚卫)
;
Fan XJ(范学军)
收藏
  |  
浏览/下载:13/0
  |  
提交时间:2021/02/01
Vibration fatigue of turbine blade for liquid rocket engine
会议论文
AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2018, 2018-01-08
作者:
Li, Y.
;
Sun, B.
;
Fang, J.
;
Liang, T.
收藏
  |  
浏览/下载:17/0
  |  
提交时间:2019/12/30
Aviation
Boosters (rocket)
Continuum damage mechanics
Fatigue of materials
Modal analysis
Rockets
Structural dynamics
Turbine components
Turbomachine blades
Damage evolution
Harmonic response analysis
Liquid rocket engines
Mechanical structures
Sinusoidal vibration
Structural fatigue
Theoretical modeling
Vibration fatigue
Vibration analysis
Parameters affecting the erosive burning of solid rocket motor
会议论文
MATEC Web of Conferences, 2017-11-28
作者:
Abdelaziz, A.
;
Guozhu, L.
;
Elsayed, A.
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  |  
浏览/下载:1/0
  |  
提交时间:2019/12/30
Product design
Propellants
Rocket engines
Rockets
Burning rate
Combustion phenomena
Erosive burning
High velocity
Motor design
Pressure-time curves
Propellant surfaces
Solid rocket motors
Composite propellants
An Adaptive Sampling Algorithm and Approximate-Model-Based Optimization Method
会议论文
Journal of Physics: Conference Series
作者:
Tian, J.L.
;
Tong, X.Y.
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  |  
浏览/下载:3/0
  |  
提交时间:2019/12/30
Computational efficiency
Learning algorithms
Machine design
Particle swarm optimization (PSO)
Rocket engines
Rockets
Adaptive sampling algorithms
Approximate model
Computation intensives
Optimization convergence
Optimization design
Sampling points
Simulation calculation
Standard test functions
Data mining
Study of cooldown thermal loading effect on the bore deformation of viscoelastic solid propellant grain
会议论文
53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017, 2017-07-10
作者:
Adel, W.M.
;
Liang, G.-Z.
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  |  
浏览/下载:7/0
  |  
提交时间:2019/12/30
Composite propellants
Propellants
Propulsion
Rocket engines
Solid propellants
Strain
Stress relaxation
Testing
Viscoelasticity
Composite solid propellant
Environmental temperature changes
Experimental approaches
Low firing temperature
Nonlinear visco-elastic
Nonlinear viscoelastic material
Thermo-structural analysis
Time-temperature superposition principles
Finite element method
Developing a viscoelastic relaxation model for AP-HTPB composite solid propellant based on experimental data
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, 2017-03-06
作者:
Adel, W.M.
;
Liang, G.-Z.
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  |  
浏览/下载:1/0
  |  
提交时间:2019/12/30
Composite propellants
HTPB propellants
Inorganic compounds
Least squares approximations
Polybutadienes
Propellants
Rocket engines
Solid propellants
Spacecraft
Spacecraft propulsion
Strain rate
Stress relaxation
Tensile testing
Viscoelasticity
3D finite element model
Composite solid propellant
Hydroxyl terminated polybutadienes
Stress relaxation data
Stress relaxation tests
Structural integrity analysis
Time dependent behavior
Viscoelastic relaxation
Finite element method
Modular simulation software development for liquid propellant rocket engines based on MATLAB Simulink
会议论文
2017 International Conference on Mechanical, Material and Aerospace Engineering, 2MAE 2017, Beijing, China, 2017-05-12
作者:
Naderi, Mahyar
;
Liang, Guozhu
;
Karimi, Hasan
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浏览/下载:2/0
  |  
提交时间:2019/12/30
Inductive Monitoring System Based Fault Detection for Liquid-Propellant Rocket Engines
会议论文
2015 34TH CHINESE CONTROL CONFERENCE (CCC), 2015-01-01
作者:
Gao Kehan
;
Xiong Zihao
;
Yi Ke
;
Dong Xiwang
;
Yang Peng
收藏
  |  
浏览/下载:8/0
  |  
提交时间:2020/01/06
Liquid-propellant rocket engine
fault detection
Inductive Monitoring System
Numerical SimulationofDirect ActionLiquid Rocket EnginesHydro mechanical Flow Controllers
会议论文
Asia-Pacific International Symposium on Aerospace Technology (APISAT), Chinese Soc Aeronaut & Astronaut, Shanghai, PEOPLES R CHINA, 2015-01-01
作者:
Bakhmet, Iana
;
Zhang Lihui
收藏
  |  
浏览/下载:1/0
  |  
提交时间:2020/01/06
flow controller
flow regulator
liquid rocket engines
dynamic characteristic
static characteristic
Time-domain numerical simulation of high frequency combustion instability in liquid propellant rocket engines
会议论文
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and exhibit 2014, Cleveland, OH, United states, 2014-07-28
作者:
Chu, Min
;
Xu, Xu
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  |  
浏览/下载:2/0
  |  
提交时间:2020/01/06
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