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Guangtao Song

Nanjing University of Aeronautics and Astronautics

H指数:6

被引数:126

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Effects of supersonic boundary layer combustion on wall shear stress and heat transfer

超音速边界层燃烧对壁面剪切应力和热传递的影响

Aerospace Science and Technology

IF5.8

2026-08-010

PRE

Thrust Loss Analysis of a Turbine-based Combined Cycle Nozzle

基于涡轮的联合循环喷管的推力损失分析

Aerospace Science and Technology

IF5.8

2025-09-170

PRE

Experimental study of influence of twin-jet interaction on over-under combined nozzle performance

双射流相互作用对上下组合喷管性能影响实验研究

Chinese Journal of Aeronautics

IF5.7

2025-06-190

OAAI

Review on the aerodynamic issues of the exhaust system for scramjet and turbine based combined cycle engine

PROGRESS IN AEROSPACE SCIENCES

IF16.2

2023-11-018

PRE

Three issues on nozzle thrust performance in cold-to-hot correlation considering variable specific heat effect

PHYSICS OF FLUIDS

IF4.3

2022-07-224

PRE

Experimental and numerical investigations on the mode transition process of an exhaust system for an over -under turbine based combined cycle

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2020-12-018

PREAI

Experimental and numerical investigations of a scramjet nozzle at various operations

超燃冲压发动机喷嘴在各种操作中的实验和数值研究

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2020-01-0113

PREAI

Design and performance analysis of an exhaust system for an over-under turbine based combined cycle operating at Mach 0-6

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2019-11-018

PREAI

Inverse design methodology on a single expansion ramp nozzle for scramjets

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2019-09-0131

PREAI