10.2. White Paper

The White Paper for Flow360 can be found here.

10.3. Rotor5: Rotor analysis under 5 hours using ultra-fast and high-fidelity CFD simulation and automatic meshing

Runda Ji, Feilin Jia, Philippe Spalart and Zongfu Yu
Flexcompute Inc, Belmont, Massachusetts, 02138
Qiqi Wang
Massachusetts Institute of Technology, Cambridge, Massachusetts 02139
Flexcompute Inc, Belmont, Massachusetts, 02138

We introduce a novel workflow called Rotor5 to simplify and accelerate the traditional high-fidelity rotor simulations by integrating (1) CAD preparation (2) mesh generation and (3) CFD solver into an end-to-end process. We quantify the limitations of a popular low-fidelity rotor design tool called Xrotor and demonstrate the necessity of using a high-fidelity CFD solver such as Rotor5. Using both Xrotor and Rotor5, we investigate the tiltrotor XV-15 at two different flight conditions: (1) airplane propeller mode in forward flight and (2) helicopter hovering mode, where the fundamental limitations of low-fidelity Xrotor could cause a catastrophic design failure. A major cause for this is the tip vortex of the preceding blade.

Full Paper

Slides

10.4. Assessment of Detached Eddy Simulation and Sliding Mesh Interface in Predicting Tiltrotor Performance in Helicopter and Airplane Modes

Feilin Jia and John Moore
Flexcompute Inc, Belmont, Massachusetts, 02138
Qiqi Wang
Massachusetts Institute of Technology, Cambridge, Massachusetts 02139

This paper presents numerical investigation on performance and flow field of the full-scale XV-15 tiltrotor in both helicopter mode (hovering flight and forward flight) and aeroplane propeller mode using Detached Eddy Simulation, in which the movement of the rotor is achieved using a Sliding Mesh Interface. Comparison of our CFD results against experiment data and other CFD results is performed and presented.

Feilin Jia, John Moore and Qiqi Wang, 2022 Assessment of Detached Eddy Simulation and Sliding Mesh Interface in Predicting Tiltrotor Performance in Helicopter and Airplane Modes

10.5. Aerodynamic Risk Assessment using Parametric, Three-Dimensional Unstructured, High-Fidelity CFD and Adaptive Sampling

Runda Ji
Flexcompute Inc, Belmont, Massachusetts, 02138
Qiqi Wang
Massachusetts Institute of Technology, Cambridge, Massachusetts 02139

We demonstrate an adaptive sampling approach for computing the probability of a rare event for a set of three-dimensional airplane geometries under various flight conditions. We develop a fully automated method to generate parameterized airplanes geometries and create volumetric mesh for viscous CFD solution. With the automatic geometry and meshing, we perform the adaptive sampling procedure to compute the probability of the rare event. We show that the computational cost of our adaptive sampling approach is hundreds of times lower than a brute-force Monte Carlo method.

Runda Ji and Qiqi Wang, 2021 Aerodynamic Risk Assessment using Parametric, Three-Dimensional Unstructured, High-Fidelity CFD and Adaptive Sampling