XV-15 Rotor Simulation in Flow360 using the Blade Element Theory

F-0078-2022-1192

5/10/2022

Authors
Abstract
Content

This paper presents results of the numerical study of the Bell XV-15 rotor with the flow solver Flow360 using a coupled Navier-Stokes/Blade Element Theory model. Results are presented for both steady-state and transient simulations. The resulting thrust, torque, and blade loadings show good agreement with high-fidelity DDES results computed with Flow360 and experiments.

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DOI
https://doi.org/10.4050/F-0078-2022-1192
Citation
Moore, J., Wang, Q., and Jia, F., "XV-15 Rotor Simulation in Flow360 using the Blade Element Theory," Vertical Flight Society 78th Annual Forum and Technology Display, Fort Worth, Texas, May 10, 2022, https://doi.org/10.4050/F-0078-2022-1192.
Additional Details
Publisher
Published
5/10/2022
Product Code
F-0078-2022-1192
Content Type
Technical Paper
Language
English