aerodynamic-analysis 话题在 GitHub 上没有填写简介，这里按 Star 数汇总最相关的热门仓库。
Aircraft design optimization made fast through computational graph transformations (e.g., automatic differentiation). Composable analysis tools for aerodynamics, propulsion, structures, trajectory design, and much more.
NeuralFoil 是一款实用的翼型空气动力学分析工具，采用基于物理的机器学习，面向终端用户，采用纯 Python/NumPy 语言。
Aerodynamic models of 3D wings using the Vortex Step Method
A mid-fidelity 3D free-wake solver for propellers, more accurate than BEMT. It simulates full wake development via a user-friendly GUI.
Flight Dynamics Project - UAV
Coaxial Helicopter Design for Helicopter Emergency Medical Services (HEMS) Operations
The study aims to develop a preliminary design of a fixed-wing aerodyne (Business Jet) able to carry a reduced number of people in intercontinental flights at the maximum possible Mach number.
Assignment Submission for the System Identification of Aerospace Vehicle (AE4320) course. Two Step Approach to Identify Aerodynamic Model - State Estimation and Parameter Estimation
CR25 SpaceConcordia 2025 solid rocketry project: a non-ordinary transition rocket due to new design required in-depth analysis. CFD simulation using OpenFOAM had been conducted to analyze aerodynamic forces on the airframe in different Angle of Attacks and Speeds
Vectorial fields in fluids simulator.
Design and development of a fixed-wing hybrid VTOL UAV, covering conceptual design, aerodynamic analysis, propulsion, structural design, flight dynamics, control, and validation.
The project aims to simulate a rocket flight from ground to the Earth orbit
RANS/SST k–ω CFD study of surface roughness effects on oblique shock formation over a double-wedge model in supersonic flow
Minimum induced drag under power-law bending constraints. A closed-form coefficient c(k) = 4(1+k)/k² unifies Prandtl's 1933 bell and Jones's 1950 root-bending result as two cases of one law, proven via the Rogers–Dougall sum and validated numerically.
Machine learning-assisted optimisation of shuttlecock porosity using Gaussian Process Regression and Bayesian optimisation
Focused on the development of a simulator that simplifies and simulates the behaviour of an AeroSail system
Post-Processing tool for 2D steady-state CFD solutions based on unstructured grids.
An interactive 3D WebGL application that accelerates aerodynamic shape evaluation by comparing a traditional 3D CFD (Computational Fluid Dynamics) Solver side-by-side with an Instant SciML (Scientific Machine Learning) Neural Surrogate.
Aerodynamics Engineer working across CFD, fluid-structure interaction, and aeroelastic flutter analysis for UAV systems. Currently at BAYKAR Technologies, building toward civil aerospace roles in Europe.
Aynı Ailden 2 Şok Dalgasının Kesişmesi Sonucu Oluşacak Akışın Genel Özelliklerini Hesaplamaktadır.