The displacement-based partitioned approach for parallel transient analysis of flexible multi-body structures

Coupled computational structural/fluid dynamics simulation for higher harmonic control of helicopter rotor

Load identification approach using structural acceleration responses based on deep learning

Preliminary Design and Characterisitcs of a Tilt Rotor Aircraft Nacelle utilizing a Tilt-rotor-only Mechanism

Surrogate Modeling Based On the Domain Decomposition Method Using the Deep Neural Network

Rotorcraft Noise Directivity Induced by Active Trailing-Edge Flap Control in Hover

Nonlinear Frequency Response Analysis Based on Hyper-Reduction approach

Three-Dimensional Flexible Multibody Dynamic Analysis Using the PartStiff Method Based on the Absolute Nodal Coordinate Formulation

Internal Structural Design Optimization for Medium-Class Helicopters through Load Path Prediction

Coupled Fluid-Structure Analysis of UH-60A Rotor via Actuator Line Method