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Nanjia Yu

beihang university

H指数:19

被引数:893

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Experimental investigation on thermal and sooting characteristics of fuel-rich LOX/kerosene combustion under varied oxidizer-to-fuel ratios

在变氧化剂-燃料比条件下对富燃料LOX/煤油燃烧的热特性和冒烟特性的实验研究

Applied Thermal Engineering

IF6.9

2026-07-011

PRE

Experimental study of partial catalytic ignition process in hydrogen peroxide/kerosene rocket engines

过氧化氢/煤油火箭发动机部分催化点火过程的实验研究

Applied Thermal Engineering

IF6.9

2025-09-230

PRE

Numerical investigation of parametric effects on the partial catalytic ignition of hydrogen peroxide/kerosene in a lab-scale rocket engine

实验室尺度火箭发动机中过氧化氢/煤油部分催化点火参数效应的数值研究

Energy Conversion and Management

IF10.9

2025-08-250

PRE

Multi-objective optimization of thrust control strategies for electric pump-fed rocket engines

电泵供液火箭发动机推力控制策略的多目标优化

Acta Astronautica

IF3.4

2025-08-250

PRE

Experimental and simulation investigation on partially catalyzed ignition process of hydrogen peroxide/kerosene in a lab-scale rocket engine

实验室规模火箭发动机中过氧化氢/煤油部分催化点火过程的实验与仿真研究

ACTA ASTRONAUTICA

IF3.4

2025-05-140

PRE

Spray characteristics of pintle injector with high gas-liquid momentum ratio

ACTA ASTRONAUTICA

IF3.4

2025-05-010

PRE

Combustion flow field and thermal protection performance of a liquid oxygen/kerosene engine with pintle injectors

ACTA ASTRONAUTICA

IF3.4

2024-12-010

PRE

Experimental study and performance analysis of a dual-mode space propulsion system pressurized by electric pump

电动泵增压双模式空间推进系统的实验研究与性能分析

ACTA ASTRONAUTICA

IF3.4

2024-11-010

PRE

Experimental study on the combustion and pressure drop characteristics of a pintle injector for LOX/kerosene rocket engine

ACTA ASTRONAUTICA

IF3.4

2024-06-012

PRE

Reduction of chemical mechanism and kinetics analysis for ignition of RP-3 aviation kerosene in partially catalyzed hydrogen peroxide

IF7.5

2024-06-014

PRE

Optimization of combustion organization scheme for pre-combustion chamber of pre-cooled engine

SCIENTIFIC REPORTS

IF3.9

2023-09-250

OAAI

The influence law of the film percentage and injection on gas film cooling effect of the liquid oxygen/methane attitude control engine

APPLIED THERMAL ENGINEERING

IF6.9

2023-02-011

PRE

2.5 kN pump-pressure pintle engine ignition experiment in different loading cases

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2022-08-015

PRE

Comparison between the dynamic characteristics of electric pump fed engine and expander cycle engine

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2022-05-0110

PRE

Experimental investigation of a flow-oriented throttleable injector designed for throttleable hybrid rocket motor

ACTA ASTRONAUTICA

IF3.4

2022-03-0117

PRE

Analysis of dynamic characteristics and sensitivity of hydrogen-oxygen expansion cycle rocket engine system

ACTA ASTRONAUTICA

IF3.4

2021-12-0115

PRE

Experimental and numerical investigations on flow field characteristics of pintle injector

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2020-08-0130

PREAI

Regression rate and combustion performance investigation on hybrid rocket motor with head-end swirl injection under high geometric swirl number

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2020-08-0132

PREAI

Numerical and experimental investigations on injection effects of orifice injector plate in hybrid rocket motors

ACTA ASTRONAUTICA

IF3.4

2019-09-0112

PREAI

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

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2018-06-0118

PREAI