Investigations using computational fluid dynamics (CFD) have been carried out on divided intake ducts having angles-of-turn as 22.5°/22.5°, 30°/30° and 45°/45° and area ratios of 2 and 3. It is observed that the core flow in the duct remains towards the convex walls up to the outlet plane with lower magnitudes in the centre of plane. Cross-velocity magnitudes are found to be less than 10 per cent of the longitudinal velocity at the outlet plane. Pressure recovery is found to decrease with the increase in the angle-of-turn for both area ratios
Demands on lower emissions and reduced noise levels drive the design of modern turbofan engines towa...
number on the critical inlet flow angle ac is calculated for diff-fusers with re/r0 = 1.2 and the re...
Integrated propulsion plays a major role in future civil and military aircraft design. A key compone...
Investigations using computational fluid dynamics (CFD) have been carried out on divided intake duct...
Investigations using computational fluid dynamics (CFD) have been carried out on divided intake duct...
Investigations carried out on divided intake ducts with 22.5°/22.5° angle-of-turn to establish the e...
Intake geometries result in unwanted secondary flows and formations of vortices which affect the eng...
To reduce fuel-burn and emissions there is a drive towards higher bypass ratio and smaller high-pres...
In the present investigation the distribution of mean velocity, static pressure and total pressure a...
317-325The flow and performance characteristics of a S-shaped diffusing duct having an area ratio of...
Intermediate turbine ducts (ITD’s) are annular S-shaped channels used in turbofan engines to guide t...
ABSTRACT Modern direct-drive turbofan engines typically have the fan turbine designed at significant...
Curved diffusers are an integral component of the gas turbine engines of high-speed aircraft. These ...
Introducing a duct along the perimeter of a rotor has been acknowledged to augment turbine performan...
Abstract: The present study involves the CFD analysis for the prediction of swirl effect on the char...
Demands on lower emissions and reduced noise levels drive the design of modern turbofan engines towa...
number on the critical inlet flow angle ac is calculated for diff-fusers with re/r0 = 1.2 and the re...
Integrated propulsion plays a major role in future civil and military aircraft design. A key compone...
Investigations using computational fluid dynamics (CFD) have been carried out on divided intake duct...
Investigations using computational fluid dynamics (CFD) have been carried out on divided intake duct...
Investigations carried out on divided intake ducts with 22.5°/22.5° angle-of-turn to establish the e...
Intake geometries result in unwanted secondary flows and formations of vortices which affect the eng...
To reduce fuel-burn and emissions there is a drive towards higher bypass ratio and smaller high-pres...
In the present investigation the distribution of mean velocity, static pressure and total pressure a...
317-325The flow and performance characteristics of a S-shaped diffusing duct having an area ratio of...
Intermediate turbine ducts (ITD’s) are annular S-shaped channels used in turbofan engines to guide t...
ABSTRACT Modern direct-drive turbofan engines typically have the fan turbine designed at significant...
Curved diffusers are an integral component of the gas turbine engines of high-speed aircraft. These ...
Introducing a duct along the perimeter of a rotor has been acknowledged to augment turbine performan...
Abstract: The present study involves the CFD analysis for the prediction of swirl effect on the char...
Demands on lower emissions and reduced noise levels drive the design of modern turbofan engines towa...
number on the critical inlet flow angle ac is calculated for diff-fusers with re/r0 = 1.2 and the re...
Integrated propulsion plays a major role in future civil and military aircraft design. A key compone...