Hot Corrosion Damage Modelling in Aero Engines Based on Performance and Flight Mission Analysis
Active Control of a Multi-Stream Rectangular Supersonic Nozzle Via Micro Jet Array
Linear and Nonlinear Stability Analysis of a Three-Dimensional Boundary Layer Over a Hump
Pressure Reconstruction from the Measured Pressure Gradient Using Gaussian Process Regression
Pressure Reconstruction from the Measured Pressure Gradient Using Gaussian Process Regression
Optimal Surface Morphing Using Adjoint Optimization
Automatic Parameterization for Aerodynamic Shape Optimization Via Deep Geometric Learning
RANS-Based Multipoint Aeropropulsive Design Optimization of an Over-Wing Nacelle Configuration
A Weakly-Coupled Simulation for HVAC Duct Aeroacoustics Including Propagation into the Cabin
An Improved What-If Post-Processing Utility – a Tribute to Dr. Garrett N. Vanderplaats