SIGLEAvailable from British Library Document Supply Centre- DSC:8019.3153(RRR-PNR--90667) / BLDSC - British Library Document Supply CentreGBUnited Kingdo
There are two main objectives associated with this research: The first portion examines the flow fie...
ObjectivesRegarding transonic flow occurring at the throat of the stator blades of axial flow turbin...
SIGLEAvailable from British Library Document Supply Centre- DSC:DX87364 / BLDSC - British Library Do...
Available from British Library Document Supply Centre- DSC:DXN055473 / BLDSC - British Library Docum...
Available from British Library Document Supply Centre-DSC:DXN025134 / BLDSC - British Library Docume...
The vibrations involved in a typical axial compressor rotor in an aircraft engine are complex. Gener...
The vibrations involved in a typical axial compressor rotor in an aircraft engine are complex. Gener...
SIGLEAvailable from British Library Document Supply Centre- DSC:9106.17(CUED/A-Turbo/TR--126) / BLDS...
SIGLEAvailable from British Library Document Supply Centre- DSC:DX79091 / BLDSC - British Library Do...
SIGLEAvailable from British Library Document Supply Centre- DSC:DX175364 / BLDSC - British Library D...
This study focuses on predicting axial compressor stage characteristics using a single performance p...
SIGLEAvailable from British Library Document Supply Centre- DSC:D68119/86 / BLDSC - British Library ...
SIGLEAvailable from British Library Document Supply Centre- DSC:DX181382 / BLDSC - British Library D...
The development of a reliable mathematical model of an axial compressor requires applying flow and e...
SIGLEAvailable from British Library Document Supply Centre-DSC:D197379 / BLDSC - British Library Doc...
There are two main objectives associated with this research: The first portion examines the flow fie...
ObjectivesRegarding transonic flow occurring at the throat of the stator blades of axial flow turbin...
SIGLEAvailable from British Library Document Supply Centre- DSC:DX87364 / BLDSC - British Library Do...
Available from British Library Document Supply Centre- DSC:DXN055473 / BLDSC - British Library Docum...
Available from British Library Document Supply Centre-DSC:DXN025134 / BLDSC - British Library Docume...
The vibrations involved in a typical axial compressor rotor in an aircraft engine are complex. Gener...
The vibrations involved in a typical axial compressor rotor in an aircraft engine are complex. Gener...
SIGLEAvailable from British Library Document Supply Centre- DSC:9106.17(CUED/A-Turbo/TR--126) / BLDS...
SIGLEAvailable from British Library Document Supply Centre- DSC:DX79091 / BLDSC - British Library Do...
SIGLEAvailable from British Library Document Supply Centre- DSC:DX175364 / BLDSC - British Library D...
This study focuses on predicting axial compressor stage characteristics using a single performance p...
SIGLEAvailable from British Library Document Supply Centre- DSC:D68119/86 / BLDSC - British Library ...
SIGLEAvailable from British Library Document Supply Centre- DSC:DX181382 / BLDSC - British Library D...
The development of a reliable mathematical model of an axial compressor requires applying flow and e...
SIGLEAvailable from British Library Document Supply Centre-DSC:D197379 / BLDSC - British Library Doc...
There are two main objectives associated with this research: The first portion examines the flow fie...
ObjectivesRegarding transonic flow occurring at the throat of the stator blades of axial flow turbin...
SIGLEAvailable from British Library Document Supply Centre- DSC:DX87364 / BLDSC - British Library Do...