Time-Domain Aeroelasticity Analysis by a Tightly Coupled Fluid-Structure Interaction Methodology
A tightly coupled fluid-structure interaction (FSI) methodology is developed for aeroelasticity analysis in the time domain. The preconditioned Navier–Stokes equations for all Mach numbers are employed and the structural equations are tightly coupled with the fluid equations by discretizing their ti...
Main Authors: | Zhongyu Liu, Xueyuan Nie, Guannan Zheng, Guowei Yang |
---|---|
Format: | Article |
Language: | English |
Published: |
MDPI AG
2021-06-01
|
Series: | Applied Sciences |
Subjects: | |
Online Access: | https://www.mdpi.com/2076-3417/11/12/5389 |
Similar Items
-
Aeroelastic Characteristics of Rotor Blades of Last Stage of a Powerful Steam Turbine
by: Liubov V. Kolodiazhna, et al.
Published: (2023-03-01) -
Aeroelastic tailoring for aerospace applications
by: Junaid Najmi, et al.
Published: (2024-01-01) -
Numerical Simulation of Tiltrotor Flow Field during Shipboard Take-Off and Landing Based on CFD-CSD Coupling
by: Peng Yu, et al.
Published: (2022-05-01) -
Aeroelastic Tailoring of the Next Generation Civil Tiltrotor Technological Demonstrator Composite Wing
by: Aniello Daniele Marano, et al.
Published: (2022-06-01) -
Effect of Aerodynamic Damping Approximations on Aeroelastic Eigensensitivities
by: Christoph Kaiser, et al.
Published: (2022-03-01)