Add to ORKGLiquid hydrogen used as heat sink for turbine cooling in high temperature turbojet engin
Methane or hydrogen fuel direct cooling of first stage stator of SST aircraft turbine - numerical he...
Given here is a definition of Liquid Air Cycle Engines (LACE) and existing relevant technologies. He...
Aviation industry is continuously growing especially for very long distance flights due to the globa...
Engineering criteria for thermodynamic improvenent of liquid hydrogen turbopumps for rocket engine
The presentation describes the recent developments in the design of the fuel and heat management sys...
Thermal conditioning problems of liquid hydrogen turbopumps to enhance mixed-phase operation and to ...
In order to meet the ambitious environmental targets set by the Paris Agreement, new sustainable car...
The potential benefits of using the fuel heat sink of hydrogen fueled supersonic transports for cool...
A series of investigations was conducted episodically from the 1950's to the early 1970's to investi...
This paper presents some results on the performance of hydrogen-based engines. In particular, the fo...
The aim of this Individual Research Project is to lay solid foundations for the investigation of liq...
Aviation industry is continuously growing especially for very long distance flights due to the globa...
Designing commercial aircraft to use liquid hydrogen (LH2) is one way to substantially reduce their ...
The High Temperature Gas-Cooled Reactor is being envisioned that will generate not just electricity,...
The effect of turbine-inlet temperature on rocket gross weight was investigated for three high-energ...
Methane or hydrogen fuel direct cooling of first stage stator of SST aircraft turbine - numerical he...
Given here is a definition of Liquid Air Cycle Engines (LACE) and existing relevant technologies. He...
Aviation industry is continuously growing especially for very long distance flights due to the globa...
Engineering criteria for thermodynamic improvenent of liquid hydrogen turbopumps for rocket engine
The presentation describes the recent developments in the design of the fuel and heat management sys...
Thermal conditioning problems of liquid hydrogen turbopumps to enhance mixed-phase operation and to ...
In order to meet the ambitious environmental targets set by the Paris Agreement, new sustainable car...
The potential benefits of using the fuel heat sink of hydrogen fueled supersonic transports for cool...
A series of investigations was conducted episodically from the 1950's to the early 1970's to investi...
This paper presents some results on the performance of hydrogen-based engines. In particular, the fo...
The aim of this Individual Research Project is to lay solid foundations for the investigation of liq...
Aviation industry is continuously growing especially for very long distance flights due to the globa...
Designing commercial aircraft to use liquid hydrogen (LH2) is one way to substantially reduce their ...
The High Temperature Gas-Cooled Reactor is being envisioned that will generate not just electricity,...
The effect of turbine-inlet temperature on rocket gross weight was investigated for three high-energ...
Methane or hydrogen fuel direct cooling of first stage stator of SST aircraft turbine - numerical he...
Given here is a definition of Liquid Air Cycle Engines (LACE) and existing relevant technologies. He...
Aviation industry is continuously growing especially for very long distance flights due to the globa...