The Single phase solver of XFlow is used by major companies in the aerospace industry. The accuracy of this solver for predicting aircraft aerodynamic behavior has been very well validated on several reference benchmarks such as the 1st and 2nd AIAA High Lift Prediction Workshops, as well as on several applications such as buffet-onset detection and post-stall conditions.
The Virtual wind Tunnel of XFlow reduces the setup time of any external aerodynamic analysis.
The interaction between aircrafts and aerodynamics is one of the new areas explored by CFD. XFlow provides the means to investigate aircraft response subject to aerodynamic loads thanks to its Rigid Body Dynamics capabilities and ability to handle arbitrary moving parts.
XFlow is capable of simulating aerospace applications involving moving parts. This unique capability allows the running of full polar sweep analysis, flaps deployment dynamics, landing gear deployment, turbofan or helicopter blade rotations and any other flight maneuvers.
XFlow enables exploration of new applications of CFD, breaking the limitations of traditional CFD solutions.
Fluid Structure Interaction
XFlow has demonstrated its ability to reproduce results of aircraft behaviors only observable in real flight conditions such as spin control, pitch damping, dutch roll, and ice shedding separation and even FSI with deformable geometries using co-simulations with Nastran, and co-simulations with external MBD software (through FMI standard) to perform complete analysis of ailerons and elevators deployment.
XFlow makes it possible to study behaviors that cannot be reproduced in wind tunnels nor in real flights test, such as aircraft ditching.
The coupling between energy and momentum equations is ensured in XFlow by several thermal models that can be used to simulate the heating, ventilation, and air conditioning system in an aircraft cabin.
Thermal post-processing is straightforward and allows visualization of the evolution of the temperature field inside the aircraft cabins, and measurement of the temperature on the passengers, on a given location using a probe, line, surface or inside a volume.
XFlow Aeroacoustics Analysis of the LAGOON Landing Gear
Aeroacoustics Analysis of the LAGOON Landing Gear using the LBM of XFlow. This video shows how the Direct Noise Computation approach of XFlow predicts very accurately the unsteady velocity field, the...
XFlow Simulation of the SYMA X8C Quadcopter with Real Rotating Blades
XFlow CFD simulation of the SYMA X8C Quadcopter drone using real rotating blades....
Articulated Body Dynamics CFD simulation of an ejection seat
The behavior of the human body subject to intense air blast is simulated during the initial stage of the ejection sequence. The effectiveness of the arm catcher is evaluated, and the forces measured...
XFlow Free-Surface Simulation of an Aircraft Water Ingestion
XFlow demonstrates in this smulations its capability to reproduce accurately a complex behavior such as aircraft water ingestion and in a very short time thanks to its quick pre-processing and its...
Spin Tunnel Test of the D-JET
The meshless CFD technology of XFlow allows complex fluid-structure interactions such as this spin tunnel test of the D-JET from Diamond Aircraft. ...
17th AIAA Aviation 2016
Non-Linear FSI using a Partitioned LBM on industrial applications: XFlow/Nastran co-simulations.
22nd AIAA/CEAS Aeroacoustics 2016
Direct Noise Computation with a Lattice-Boltzmann Method and Application to Industrial Test Cases.
18th International Conference on CFD 2016
Prediction of Finned Projectile Aerodynamics behavior at Mach 0.5, 0.6 and 0.7 using a Lattice-Boltzmann Method CFD Solution.
NAFEMS Benchmark magazine publication
The paper that won the “Best Presented Paper” award at the 2013 NAFEMS World Congress.
NAFEMS World Congress 2015
>Stall Prediction of the Piaggio Aerospace P1XX Aircraft Using a Lattice-Boltzmann Method Solution
AIAA AVIATION 2014
Aerodynamic analysis of the 2nd High Lift Prediction Workshop by a Lattice-Boltzmann Method solver
2nd AIAA High Lift Prediction Workshop
Lattice-Boltzmann Contribution to the 2nd AIAA High Lift Prediction Workshop
NAFEMS World Congress 2013
Dynamic Simulation of Flight Test Manoeuvres on the Diamond D-JET
AIAA 2012 XFlow Presentation
Advanced Aerodynamic Analysis of the NASA High-Lift Trap Wing with a Moving Flap Configuration
1st AIAA High Lift Prediction Workshop
XFlow CFD results for the 1st AIAA High Lift Prediction Workshop.
NAFEMS 2011 XFlow Presentation
Aerodynamic analysis involving moving parts with a particle-based CFD solution.