Validation of the EFEA Method through Correlation with Conventional FEA and SEA Results
Robust Flight Controller Design Based on Adaptive Nonlinear Dynamic Inverse with Reference Model
Research and Application of Fault Diagnosis Method Based on Time Fault Propagation Graph
Reconstruction of Noise Source in a Ducted Fan Using a Generalized Nearfield Acoustical Holography
Powertrain Mounting System with Uncertainty Using Chebyshev Interval Method
Optimization of a Porous Ducted Air Induction System Using Taguchi's Parameter Design Method
Model Order Reduction Using Basis Expansions for Near field Acoustic Holography
Influence of Continuous Jet at the Lower Surface on Airfoil Aerodynamic Performance