The paper describes an analysis method for an inertial particle separator (IPS) system modeled as a multi-element airfoil configuration. The analysis method is implemented in a numerical tool that is able to perform impingement analysis using spherical, non-spherical particles as well as water droplets for a range of Reynolds number (10-4 ≤ Re ≤ 5×105). A limitations of the analysis tool is that it lacks an appropriate particle rebound model for the treatment of particle-wall collisions. The usefulness of the analysis tool is its use in conjunction with a multipoint inverse design tool for the design of multi-element airfoil based IPS system model in an inverse fashion as opposed to the direct design methods being employed currently for thi...
Computational analysis of particle-laden-airflow erosion can help engineers have a better understand...
This study was conducted to provide a new possible approach to the designing process of an airfoil. ...
The effectiveness of a typical helicopter particle separation system has been numerically assessed a...
The paper describes an analysis method for an inertial particle separator (IPS) system modeled as a ...
This paper presents research into practical simulations of particle flow in inertial particle separa...
This paper presents research into practical simulations of particle flow in inertial particle separa...
This thesis focuses on ingestion of foreign objects into standard turboprop engine GE H80 situated i...
Abstract—This paper presents the details of development of an efficient interactive design tool for ...
A 3-dimensional particle trajectory computer code was developed to compute the distribution of water...
Inertial Particle Separators are utilized in the inlet of a gas turbine engine to remove a significa...
General aviation aircraft and helicopters exposed to an icing environment can accumulate ice resulti...
Solid particles, such as sand, ingested into gas turbine engines, reduce the coolant flow in the tur...
A particle tracking code is presented to compute droplet trajectories within a known Eulerian flo...
cited By 66In this article, we present numerical solutions for flow over an airfoil and a square obs...
As the need for personal air transport increases significantly, new aircraft and/or its components a...
Computational analysis of particle-laden-airflow erosion can help engineers have a better understand...
This study was conducted to provide a new possible approach to the designing process of an airfoil. ...
The effectiveness of a typical helicopter particle separation system has been numerically assessed a...
The paper describes an analysis method for an inertial particle separator (IPS) system modeled as a ...
This paper presents research into practical simulations of particle flow in inertial particle separa...
This paper presents research into practical simulations of particle flow in inertial particle separa...
This thesis focuses on ingestion of foreign objects into standard turboprop engine GE H80 situated i...
Abstract—This paper presents the details of development of an efficient interactive design tool for ...
A 3-dimensional particle trajectory computer code was developed to compute the distribution of water...
Inertial Particle Separators are utilized in the inlet of a gas turbine engine to remove a significa...
General aviation aircraft and helicopters exposed to an icing environment can accumulate ice resulti...
Solid particles, such as sand, ingested into gas turbine engines, reduce the coolant flow in the tur...
A particle tracking code is presented to compute droplet trajectories within a known Eulerian flo...
cited By 66In this article, we present numerical solutions for flow over an airfoil and a square obs...
As the need for personal air transport increases significantly, new aircraft and/or its components a...
Computational analysis of particle-laden-airflow erosion can help engineers have a better understand...
This study was conducted to provide a new possible approach to the designing process of an airfoil. ...
The effectiveness of a typical helicopter particle separation system has been numerically assessed a...