Investigations carried out on divided intake ducts with 22.5°/22.5° angle-of-turn to establish the effect of Reynolds number (Re = 6.27 · 104 to 1.88 · 105) and area ratios (2.0 to 4.0) using Computational Fluid Dynamics (CFD) code are reported. The core flow remains close to the convex wall at the duct outlet with magnitudes lower in the central region of the cross-section. It is found that static pressure recovery is around 65% and is independent of inlet Reynolds number for area ratio 2 duct (AR = 2). With increase in area ratio the static pressure recovery increases to 74% for AR = 2.5, 78% for AR = 3 and 80 % for AR = 4. The cross-velocity magnitudes at the exit for all the cases are found to be less than 5 % of the mean flow
number on the critical inlet flow angle ac is calculated for diff-fusers with re/r0 = 1.2 and the re...
© 2020 St-Petersburg State Polytechnical University. All rights reserved. Subject. In technological ...
Introducing a duct along the perimeter of a rotor has been acknowledged to augment turbine performan...
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...
In the present investigation the distribution of mean velocity, static pressure and total pressure a...
In the present investigation the distribution of mean velocity, static pressure and total pressure a...
To reduce fuel-burn and emissions there is a drive towards higher bypass ratio and smaller high-pres...
An investigation was conducted to determine the effect of the inlet Mach number and entrance-boundar...
Intake geometries result in unwanted secondary flows and formations of vortices which affect the eng...
A proven duct flow model is used to examine the influence of the intake duct geometric and inlet flo...
ABSTRACT Modern direct-drive turbofan engines typically have the fan turbine designed at significant...
Abstract-- In the present investigation the distribution of mean velocity, static pressure and total...
This paper presents the Computational Fluid Dynamic (CFD) analysis to study the effect of area ratio...
Curved diffusers are an integral component of the gas turbine engines of high-speed aircraft. These ...
number on the critical inlet flow angle ac is calculated for diff-fusers with re/r0 = 1.2 and the re...
© 2020 St-Petersburg State Polytechnical University. All rights reserved. Subject. In technological ...
Introducing a duct along the perimeter of a rotor has been acknowledged to augment turbine performan...
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...
In the present investigation the distribution of mean velocity, static pressure and total pressure a...
In the present investigation the distribution of mean velocity, static pressure and total pressure a...
To reduce fuel-burn and emissions there is a drive towards higher bypass ratio and smaller high-pres...
An investigation was conducted to determine the effect of the inlet Mach number and entrance-boundar...
Intake geometries result in unwanted secondary flows and formations of vortices which affect the eng...
A proven duct flow model is used to examine the influence of the intake duct geometric and inlet flo...
ABSTRACT Modern direct-drive turbofan engines typically have the fan turbine designed at significant...
Abstract-- In the present investigation the distribution of mean velocity, static pressure and total...
This paper presents the Computational Fluid Dynamic (CFD) analysis to study the effect of area ratio...
Curved diffusers are an integral component of the gas turbine engines of high-speed aircraft. These ...
number on the critical inlet flow angle ac is calculated for diff-fusers with re/r0 = 1.2 and the re...
© 2020 St-Petersburg State Polytechnical University. All rights reserved. Subject. In technological ...
Introducing a duct along the perimeter of a rotor has been acknowledged to augment turbine performan...