Pinned Repositories
2D_CARFIVE
2D Cartesian Quadtree Adaptive Mesh Refinement (AMR) for multiphase Five Equations Model
30min_guides
覃健祥的学习笔记，各种几十分钟入门的文档
ABAQUS
ABAQUS subroutines
Aerodynamic-Shape-Optimization-of-Savonius-Wind-Turbines-using-Genetic-Algorithm
The source code related to my MPhil research
AMR_Sipp_Schmid_2016
Freefem++ and Matlab codes described in Sipp and Schmid, "Linear Closed-Loop Control of Fluid Instabilities and Noise-Induced Perturbations: A Review of Approaches and Tools", Applied Mechanics Reviews, 2016.
amrex
Block-Structured AMR Framework
anotherFEM
Finite element framework written in Fortran 2008, following object-oriented programming paradigm
ATAP
MATLAB M-files for _Approximation Theory and Approximation Practice_
mono-component-droplet
UDF for heating and evaporation of an n-dodecane/isooctane/water droplet
NASTRAN-95
rocky420's Repositories
rocky420/Blade-Element-Theory
Computation of multirotor UAV rotor forces based on Blade Element Theory
rocky420/Blade-element-theory-solver
Solver for computing propeller performance characteristics using Blade Element Theory
rocky420/coarse_to_fine_DIOF
dynamic illumination optical flow computing
rocky420/coarse_to_fine_HS_PIV
coarse-to-fine variational optical flow method for fluid flows
rocky420/crazyswarm
A Large Quadcopter Swarm
rocky420/Cylinder2DFlowControlDRL
code for performing active flow control of the 2D Karman street using Deep Reinforcement Learning
rocky420/download
Lantern官方版本下载 蓝灯 翻墙 代理 科学上网 外网 加速器 梯子 路由 proxy vpn circumvention gfw
rocky420/FBoxLib
Fortran BoxLib
rocky420/Ffowcs-Williams-and-Hawkings-Equations
Open source codes/programs of acoustic analogies to calculate subsonic and supersonic noise characteristics induced by unsteady flow, moving geometry and mutual interactions either in a stationary or a moving medium. A permeable interface with arbitrary mesh is adopted to enclose the nonlinear region calculated by unsteady CFD solvers (Fluent).
rocky420/FLOWUnsteady
Mixed-fidelity unsteady aerodynamics and aeroacoustics
rocky420/FLUSI
Fluid-Structure-Interaction / MHD Research Code. Relies on Fourier transforms for derivatives and the volume penalization method to include obstacles.
rocky420/GEBTAero
High-aspect-ratio composite wing nonlinear aeroelastic toolbox
rocky420/Incompact3d
New version of our solver for the incompressible Navier-Stokes equations
rocky420/lesgo
The Large-Eddy Simulation framework from the Turbulence Research Group at Johns Hopkins University
rocky420/MFC-Caltech
High-fidelity multiphase flow simulation
rocky420/ning2020-bem
Scripts to reproduce results in "Using Blade Element Momentum Methods with Gradient-Based Design Optimization"
rocky420/OFF
OFF, Open source Finite volume Fluid dynamics code
rocky420/piclas
PICLas is a parallel, three-dimensional PIC-DSMC solver developed cooperatively by the Institute of Space Systems, Institute of Aerodynamics and Gas Dynamics at the University of Stuttgart and the spin-off boltzplatz. PICLas is a flexible particle-based plasma simulation suite.
rocky420/PIV_dataset
PIV dataset
rocky420/PX4Firmware
PX4 Pro Autopilot Software
rocky420/PyDMD
Python Dynamic Mode Decomposition
rocky420/QTAdaptive
Quadtree Adaptive Mesh Refinement
rocky420/rbf
Mode shape interpolation via radial basis functions
rocky420/resolvent
Repository for all Matlab/Python code for the Navier-Stokes Resolvent analysis
rocky420/ROM_code
Numerical tool for Construction of Reduced-order models for fluid flows.
rocky420/sharpy
Simulation of High Aspect Ratio aeroplanes in Python: a nonlinear aeroelastic code
rocky420/sqgmu
rocky420/T-Blade3
T-Blade3 VERSION 1.2: T-Blade3 is a general parametric 3D blade geometry builder. The tool can create a variety of 3D blade geometries based on few basic parameters and limited interaction with a CAD system. The geometric and aerodynamic parameters are used to create 2D airfoils and these airfoils are stacked on the desired stacking axis. The tool generates a specified number of 2D blade sections in a 3D Cartesian coordinate system. The geometry modeler can also be used for generating 3D blades with special features like bent tip, split tip and other concepts, which can be explored with minimum changes to the blade geometry. The use of control points for the definition of splines makes it easy to modify the blade shapes quickly and smoothly to obtain the desired blade model. The second derivative of the mean-line (related to the curvature) is controlled using B-splines to create the airfoils. This is analytically integrated twice to obtain the mean-line. A smooth thickness distribution is then added to the airfoil with two options either the Wennerstrom distribution or a quartic B-spline thickness distribution. B-splines have also been implemented to achieve customized airfoil leading and trailing edges.
rocky420/Thesis
Documentation, code and writeup for my thesis: Acoustic Scattering in Shear Flow
rocky420/Wing-Flutter