CFD Labcompleted
CFD Lab: Convergent-Divergent Nozzle Flow
AE 4699 nozzle-flow assignment using ANSYS Fluent to capture choking behavior and supersonic acceleration in a convergent-divergent geometry.
Tools / Stack
ANSYS FluentCompressible FlowPost-Processing View projectCFD Labcompleted
CFD Lab: Supersonic Flow Over a Wedge
Supersonic wedge study following the Ansys Innovation lesson workflow, with wedge/cone contour comparisons for shock-driven density, pressure, and Mach behavior.
Tools / Stack
ANSYS FluentCompressible FlowOblique Shock AnalysisPost-Processing View projectCFD Labcompleted
CFD Lab: Transonic NACA 0012 Airfoil Analysis
AE 4699 transonic airfoil assignment using ANSYS Fluent to study Mach and pressure-field behavior with validation-oriented coefficient reporting.
Tools / Stack
ANSYS FluentAirfoil CFDCompressible Aerodynamics View project