A prerequisite for the prediction of ice accretion on an aircraft flying through clouds of supercooled liquid water is the accurate determination of the water impingement rate on various components of the aircraft. For this purpose, a droplet impingement module has been developed using the datastructure of the unstructured Navier-Stokes solver TAU. Since nowadays large computational grids are common practice, an efficient algorithm for determination of the droplet trajectories on such grids had to be implemented. This paper describes the physics and details of the implemented numerical algorithm. It summarizes lessons learned during development. The paper concludes with the presentation of code validation results and examples o...
In this study, computational methods are presented that compute ice accretion on multiple-element ai...
In-flight ice accretion may possibly jeopardize the safety of fixed-and rotary-wing aircraft. Icing ...
Droplet trajectories about a sphere in ideal fluid flow were calculated. From the calculated droplet...
A prerequisite for the prediction of ice accretion on an aircraft flying through clouds of supercool...
A particle tracking code is presented to compute droplet trajectories within a known Eulerian flo...
A particle tracking framework for the computation of the collection efficiency for in-flight ice acc...
The objective of this work is to present a three-dimensional Euler-Euler finite volume poly-disperse...
When trying to predict how and where ice will accrete on an aircraft, engineers first need to be abl...
In the current article, continued efforts to improve a computational in-flight ice accretion predict...
A three-dimensional Eulerian analysis has been developed for modeling droplet impingement on lifting...
A grid block transformation scheme which allows the input of grids in arbitrary reference frames, th...
Computer simulations of the ice accretion process provide an attractive method for analyzing a wide ...
This document is the Accepted Manuscript version of the following article: C. Wang, S. Chang, and H....
General aviation aircraft and helicopters exposed to an icing environment can accumulate ice resulti...
This paper focuses on the solution of the dispersed phase of Eulerian–Lagrangian one-way coupled par...
In this study, computational methods are presented that compute ice accretion on multiple-element ai...
In-flight ice accretion may possibly jeopardize the safety of fixed-and rotary-wing aircraft. Icing ...
Droplet trajectories about a sphere in ideal fluid flow were calculated. From the calculated droplet...
A prerequisite for the prediction of ice accretion on an aircraft flying through clouds of supercool...
A particle tracking code is presented to compute droplet trajectories within a known Eulerian flo...
A particle tracking framework for the computation of the collection efficiency for in-flight ice acc...
The objective of this work is to present a three-dimensional Euler-Euler finite volume poly-disperse...
When trying to predict how and where ice will accrete on an aircraft, engineers first need to be abl...
In the current article, continued efforts to improve a computational in-flight ice accretion predict...
A three-dimensional Eulerian analysis has been developed for modeling droplet impingement on lifting...
A grid block transformation scheme which allows the input of grids in arbitrary reference frames, th...
Computer simulations of the ice accretion process provide an attractive method for analyzing a wide ...
This document is the Accepted Manuscript version of the following article: C. Wang, S. Chang, and H....
General aviation aircraft and helicopters exposed to an icing environment can accumulate ice resulti...
This paper focuses on the solution of the dispersed phase of Eulerian–Lagrangian one-way coupled par...
In this study, computational methods are presented that compute ice accretion on multiple-element ai...
In-flight ice accretion may possibly jeopardize the safety of fixed-and rotary-wing aircraft. Icing ...
Droplet trajectories about a sphere in ideal fluid flow were calculated. From the calculated droplet...