Industry-Grade External Aerodynamics - Geometry to Experimental Validation
ANSYS Fluent | Subsonic to Supersonic | Mesh Generation to Result Validation | Industry Best Practices
Pre-simulation decision framework for external aerodynamics CFD - flow regime classification, solver and turbulence selection, convergence strategy, and interview preparation.
Production-ready DLR-F6 wing-body external aerodynamics CFD - geometry preparation through solver setup, post-processing, and experimental validation with y⁺ ≤ 1 transition modeling.
Production-ready polyhedral mesh generation for the NASA Canard Control Missile using custom ANSYS Fluent console commands - full control over every meshing decision on a supersonic benchmark case.
Mach 3.5 supersonic solver setup for the NASA Canard Control Missile - CN/CA coefficient extraction and validation against NASA wind tunnel data at 18 degrees angle of attack.
Complete NACA 4-(3)(08)-03 research propeller external aerodynamics CFD - Reference Frame Motion Modeling, periodic sector domain, and thrust validation against published NACA experimental data.
Complete 1-way FSI workflow in Ansys Workbench - theory of fluid-structure coupling, Static Data Transfer vs System Coupling, and hands-on flow probe simulation at 100 m/s.
Industry-Grade External Aerodynamics - Geometry to Experimental Validation
ANSYS Fluent | Subsonic to Supersonic | Mesh Generation to Result Validation | Industry Best Practices
Pre-simulation decision framework for external aerodynamics CFD - flow regime classification, solver and turbulence selection, convergence strategy, and interview preparation.
Production-ready DLR-F6 wing-body external aerodynamics CFD - geometry preparation through solver setup, post-processing, and experimental validation with y⁺ ≤ 1 transition modeling.
Production-ready polyhedral mesh generation for the NASA Canard Control Missile using custom ANSYS Fluent console commands - full control over every meshing decision on a supersonic benchmark case.
Mach 3.5 supersonic solver setup for the NASA Canard Control Missile - CN/CA coefficient extraction and validation against NASA wind tunnel data at 18 degrees angle of attack.
Complete NACA 4-(3)(08)-03 research propeller external aerodynamics CFD - Reference Frame Motion Modeling, periodic sector domain, and thrust validation against published NACA experimental data.
Complete 1-way FSI workflow in Ansys Workbench - theory of fluid-structure coupling, Static Data Transfer vs System Coupling, and hands-on flow probe simulation at 100 m/s.