Asia-Pacific Region's Aircraft Design and Development Strategy for Single-Aisle Aircraft in the Oligopoly Market of Boeing and Airbus -- Study on wind resistance characteristics of Multi-rotor UAV -- Inverse Design Method of Transonic Airfoil Based on Deep Neural Network,- High-rise Building Wind Field Simulation -- Study on Aerodynamic Characteristics of "Propeller/Wing" System with Overset Meshes Method -- An Ontology Based Single Source of Truth (SSOT) Construction Approach for Aircraft Modeling and Simulation -- Experimental Investigations on Aerodynamic and Psychoacoustic Characteristics of Loop-Type Propeller -- Effect of Dynamic Micro Vortex Generator on Corner Shock Wave Boundary Layer Interactions Based on DES -- Aerodynamic Characteristics of a Compound Deflected LEF/TEF Rotor -- Analysis of Aerodynamic Characteristics and Influence of Parameters of the Quad Tiltrotor Aircraft -- A Two-step Optimization Method Using POD-based GeometricParameterization for Aerodynamic Shape Optimization -- Anti-Icing Performance of Engine Inlet Cone by Hot Air Film -- Aerodynamic characteristics of close UAV formation -- Conceptual design and system level analysis of tilt-duct eVTOL aircraft -- Research on Wind Tunnel Test of the Total Pressure Probe Layout for Civil Aircraft -- Study on the Dynamic Aerodynamic Performance of Airfoil with Direct Force Measurement -- The Research of Correlationship and Critical Ice Shape Acquisition in CIRA-IWT Icing Wind Tunnel.