Fluent Aero is an advanced software for aerodynamic flow simulations, designed to automate the process with high precision. It simplifies the setup by automatically adjusting angles of attack and Mach numbers, requiring only the Mach number range, reference area, reference length, freestream pressure, and temperature from the user. The software handles the rest, including angle of attack and Mach number adjustments, without needing separate x and y components.
Fluent Aero is an advanced software for aerodynamic flow simulations, designed to automate the process with high precision. It simplifies the setup by automatically adjusting angles of attack and Mach numbers, requiring only the Mach number range, reference area, reference length, freestream pressure, and temperature from the user. The software handles the rest, including angle of attack and Mach number adjustments, without needing separate x and y components.
Fluent Aero utilizes the Fluent solver’s features to achieve accurate results with fewer iterations and provides comprehensive outputs, including aerodynamic coefficients and residuals plots in Excel format for easy analysis.
In this course, we'll use the Fluent Aero will manage the simulation with minimal setup, and we'll compare the results, such as drag, lift, and moment coefficients, against NASA’s
7 - 0.92) and boundary layer separation. Designed by ONERA in 1972, it serves as a model for studying high Reynolds number flows with a swept-back wing.
Course Resources:
PowerPoint slides
AGARD Report
NASA paper
Mesh file
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