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Dynamic reliability analysis for the reusable thrust chamber: A multi-failure modes investigation based on coupled thermal-structural analysis

Reliability engineering & system safety, 2020-12, Vol.204, p.107080, Article 107080

2020

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Molecular dynamics simulation of ionic liquid electrospray: Revealing the effects of interaction potential models

Acta astronautica, 2021-02, Vol.179, p.581-593

2021

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Design optimization and analysis of HTHL suborbital spaceplanes propelled by hybrid rocket motors

Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 2023-06, Vol.237 (7), p.1637-1653

2023

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Uncertainty analysis and design optimization of solid rocket motors with finocyl grain

Structural and multidisciplinary optimization, 2020-12, Vol.62 (6), p.3521-3537

2020

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Flow structures and wall parameters on rotating riblet disks and their effects on drag reduction

Alexandria engineering journal, 2022-04, Vol.61 (4), p.2673-2686

2022

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Active Fault-Tolerant Control for Quadrotor UAV against Sensor Fault Diagnosed by the Auto Sequential Random Forest

Aerospace, 2022-09, Vol.9 (9), p.518

2022

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Starting and Regulating Characteristics of Electric Pump Feed System for LRE under Different Schemes

Applied sciences, 2022-07, Vol.12 (13), p.6441

2022

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Research on copper erosion in hydrogen peroxide/kerosene bipropellant thrust chamber

Acta astronautica, 2021-11, Vol.188, p.252-264

2021

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Aerodynamic Thermal Simulation and Heat Flux Distribution Study of Mechanical Expansion Reentry Vehicle

Aerospace, 2023-03, Vol.10 (3), p.310

2023

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Hybrid uncertainty-based design optimization and its application to hybrid rocket motors for manned lunar landing

Chinese journal of aeronautics, 2017-04, Vol.30 (2), p.719-725

2017

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Effects of wall conditions on flow field in a circular micro-channel

Applied thermal engineering, 2016-10, Vol.109, p.217-226

2016

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A Review of Research on the Vacuum Plume

Aerospace, 2022-11, Vol.9 (11), p.706

2022

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Sequence-to-Sequence Remaining Useful Life Prediction of the Highly Maneuverable Unmanned Aerial Vehicle: A Multilevel Fusion Transformer Network Solution

Mathematics (Basel), 2022-05, Vol.10 (10), p.1733

2022

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Analysis of influencing parameters in ion thruster plume simulation

Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 2021-08, Vol.235 (10), p.1158-1169

2021

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Low-pressure adsorption isotherms of CO2 on low-temperature surface measured on a quartz crystal microbalance

Vacuum, 2019-10, Vol.168, p.108851, Article 108851

2019

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Research Progress on Active Secondary Jet Technology in Supersonic Flow Field of Aerospace Propulsion Systems

Fluids (Basel), 2023-12, Vol.8 (12), p.313

2023

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Static Equilibrium Characteristics of Full‐Flow Staged Combustion Cycle Engine Under Different Propellants

International Journal of Aerospace Engineering, 2024-09, Vol.2024 (1)

2024

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Enhancing payload capacity to low earth orbit via a relay solution trajectory with laser-powered vehicles

Geo-spatial information science, 2024-07, p.1-20

2024

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Three-dimensional particle simulation of back-sputtered carbon in electric propulsion test facility

Acta astronautica, 2017-03, Vol.132, p.161-169

2017

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Structural Dynamic Model Updating with Automatic Mode Identification Using Particle Swarm Optimization

Applied sciences, 2022-09, Vol.12 (18), p.8958

2022

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Design and experimental research of a sub-Newton N2O monopropellant thruster with inner-heater

Chinese journal of aeronautics, 2022-05, Vol.35 (5), p.309-318

2022

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Experimental Investigation of Combustion in Axial-Injection End-Burning Hybrid Rocket Motor

Journal of propulsion and power, 2015-05, Vol.31 (3), p.930-936

2015

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An Application of Analytical Target Cascading for a Hierarchical Multidisciplinary System: The Preliminary Design of a Launch Vehicle Powered by Hybrid Rocket Motors

Aerospace, 2022-12, Vol.9 (12), p.778

2022

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Index allocation for a reusable LOX/CH4 rocket engine

Chinese journal of aeronautics, 2021-02, Vol.34 (2), p.432-440

2021

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Experimental and numerical investigation of combustion characteristics on GO2/GH2 shear coaxial injector

Aerospace science and technology, 2018-06, Vol.77, p.725-732

2018

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Dynamic reliability analysis for the reusable thrust chamber: A multi-failure modes investigation based on coupled thermal-structural analysis

Molecular dynamics simulation of ionic liquid electrospray: Revealing the effects of interaction potential models

Design optimization and analysis of HTHL suborbital spaceplanes propelled by hybrid rocket motors

Uncertainty analysis and design optimization of solid rocket motors with finocyl grain

Flow structures and wall parameters on rotating riblet disks and their effects on drag reduction

Active Fault-Tolerant Control for Quadrotor UAV against Sensor Fault Diagnosed by the Auto Sequential Random Forest

Starting and Regulating Characteristics of Electric Pump Feed System for LRE under Different Schemes

Research on copper erosion in hydrogen peroxide/kerosene bipropellant thrust chamber

Aerodynamic Thermal Simulation and Heat Flux Distribution Study of Mechanical Expansion Reentry Vehicle

Hybrid uncertainty-based design optimization and its application to hybrid rocket motors for manned lunar landing

Effects of wall conditions on flow field in a circular micro-channel

A Review of Research on the Vacuum Plume

Sequence-to-Sequence Remaining Useful Life Prediction of the Highly Maneuverable Unmanned Aerial Vehicle: A Multilevel Fusion Transformer Network Solution

Analysis of influencing parameters in ion thruster plume simulation

Low-pressure adsorption isotherms of CO2 on low-temperature surface measured on a quartz crystal microbalance

Research Progress on Active Secondary Jet Technology in Supersonic Flow Field of Aerospace Propulsion Systems

Static Equilibrium Characteristics of Full‐Flow Staged Combustion Cycle Engine Under Different Propellants

Enhancing payload capacity to low earth orbit via a relay solution trajectory with laser-powered vehicles

Three-dimensional particle simulation of back-sputtered carbon in electric propulsion test facility

Structural Dynamic Model Updating with Automatic Mode Identification Using Particle Swarm Optimization

Design and experimental research of a sub-Newton N2O monopropellant thruster with inner-heater

Experimental Investigation of Combustion in Axial-Injection End-Burning Hybrid Rocket Motor

An Application of Analytical Target Cascading for a Hierarchical Multidisciplinary System: The Preliminary Design of a Launch Vehicle Powered by Hybrid Rocket Motors

Index allocation for a reusable LOX/CH4 rocket engine

Experimental and numerical investigation of combustion characteristics on GO2/GH2 shear coaxial injector

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