Referees for CodinGame multiplayers
A panel-based flow solver. Currently in beta but with working solvers for incompressible and inviscid hypersonic flow.
Python package which allows a user to generate waverider geometries
6-DoF hypersonic vehicle flight dynamics model coupled with a one-dimensional scramjet thermodynamic engine, including integrated guidance, navigation, and control.
Aniray is a library for animating and orchestrating large arrays of emitters, actuators, displays, and more
Using filtering techniques to smoothen hyper-sonic shockwave in MATLAB
Comparison between the flow field around a cone (3D) and a wedge (2D). Analysis of the Taylor-Maccoll flow field within the supersonic boundary layer of a cone at zero angle of attack in a hypersonic flow.
Automated calibration of RANS turbulence models for hypersonic flows using SciML. Achieved 61.3% RMSE reduction at Mach 14.
Matlab code for the determination of the reentry trajectory, deceleration profiles, and heat flux of the ARD capsule during orbital reentry into Earth's atmosphere.
Mach-4 supersonic-intake shock-wave / boundary-layer transition case study computed with the UniSTAR-CFD solver, validated against three real experimental benchmarks.
CFD investigation of hypersonic airfoil configurations using ANSYS Fluent
AI-driven aerodynamic analysis of scramjet hypersonic vehicle using OpenVSP VSPAERO PrePoMax and ML
Hermeus — independent third-party profile of a public API surface, by API Evangelist. Hermeus is an American aerospace and defense company building rapidly reusable high-Mach and hypersonic aircraft for national-security missions in partnership with the U.S. Department of Defense.
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