Institute of Aerodynamics and Gas Dynamics

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1 to 10 of 447 Results

01_cylinder.zip Jul 22, 2026 - Supplementary Material: A Provably Robust Multi-Jet Framework applied to Active Flow Control of an Airfoil in Weakly Compressible Flow ZIP Archive - 17.5 MB - MD5: f752fce35748591e163cadf4b9a5127a
02_airfoil.zip Jul 22, 2026 - Supplementary Material: A Provably Robust Multi-Jet Framework applied to Active Flow Control of an Airfoil in Weakly Compressible Flow ZIP Archive - 95.7 MB - MD5: 4fd98ce005a56bacf4e560a2e8b62bc9
build.py Jul 22, 2026 - Supplementary Material: A Provably Robust Multi-Jet Framework applied to Active Flow Control of an Airfoil in Weakly Compressible Flow Python Source Code - 5.4 KB - MD5: c220e07653c938bb2c136b9e1c6450e1
README Jul 22, 2026 - Supplementary Material: A Provably Robust Multi-Jet Framework applied to Active Flow Control of an Airfoil in Weakly Compressible Flow Plain Text - 1.1 KB - MD5: 11823b329e52e86ce07840d5560324e8
userblock.tmp Jul 22, 2026 - Supplementary Material: A Provably Robust Multi-Jet Framework applied to Active Flow Control of an Airfoil in Weakly Compressible Flow Unknown - 4.0 KB - MD5: ab9876d37aa541ae75e2d6f28e7838c7
bl022_3Dpolars_and_data.tar.bz2 Jul 10, 2026 - Data for: Transforming Laser-Scanned 750 kW Turbine Surface Geometry Data into Smooth CAD for CFD Simulations Bzip Archive - 823.9 KB - MD5: 27d1f94a407bdd52e329b0bdb6b5b3d6 Airfoil tables [lift, drag and moment coefficients]; blade properties [radius, chord, twist] and airfoil coordinates; for the 193 cross-sectional segments of blade 022 of the southern wind turbine at the WINSENT test site; see the technical note (technical-note-3Dpolars_C.pdf) for more information
technical-note-3Dpolars_C.pdf Jul 10, 2026 - Data for: Transforming Laser-Scanned 750 kW Turbine Surface Geometry Data into Smooth CAD for CFD Simulations Adobe PDF - 1.2 MB - MD5: 81a2a4ad2420975bee403844cc88dd08 This document describes the method used to obtain the airfoil tables (polars) for lift, drag, and moment using 3D URANS CFD on 193 segments for blade 022 within a one-third turbine model simulation.
technical-note-polar_twists_chord_Reynolds.pdf Jul 10, 2026 - Data for: Transforming Laser-Scanned 750 kW Turbine Surface Geometry Data into Smooth CAD for CFD Simulations Adobe PDF - 1.0 MB - MD5: 01149853bb4abc92a0416d16eb9cbffc This document explains how to properly use the WINSENT airfoil aerodynamic tables (polars), with an emphasis on the twist, chord and Reynolds number distributions of each polar set. A method is also given to adjust the polars to a different twist and chord distribution, or to compare polar sets generated with different distributions.
glxiv2_single_node_fv_pid_tts_cpu_vs_gpu.csv Jun 1, 2026 - GALÆXI v2.0: Performance Comma Separated Values - 253 B - MD5: da9d10167b611a6381b21d96773f34a6
glxiv2_single_node_power_to_solution_lumi_mn5.csv Jun 1, 2026 - GALÆXI v2.0: Performance Comma Separated Values - 155 B - MD5: 7b787bc080d956aafc433f0c5b5a63ee

01_cylinder.zip

Jul 22, 2026 - Supplementary Material: A Provably Robust Multi-Jet Framework applied to Active Flow Control of an Airfoil in Weakly Compressible Flow

ZIP Archive - 17.5 MB -

02_airfoil.zip

Jul 22, 2026 - Supplementary Material: A Provably Robust Multi-Jet Framework applied to Active Flow Control of an Airfoil in Weakly Compressible Flow

ZIP Archive - 95.7 MB -

build.py

Jul 22, 2026 - Supplementary Material: A Provably Robust Multi-Jet Framework applied to Active Flow Control of an Airfoil in Weakly Compressible Flow

Python Source Code - 5.4 KB -

README

Jul 22, 2026 - Supplementary Material: A Provably Robust Multi-Jet Framework applied to Active Flow Control of an Airfoil in Weakly Compressible Flow

Plain Text - 1.1 KB -

userblock.tmp

Jul 22, 2026 - Supplementary Material: A Provably Robust Multi-Jet Framework applied to Active Flow Control of an Airfoil in Weakly Compressible Flow

Unknown - 4.0 KB -

bl022_3Dpolars_and_data.tar.bz2

Jul 10, 2026 - Data for: Transforming Laser-Scanned 750 kW Turbine Surface Geometry Data into Smooth CAD for CFD Simulations

Bzip Archive - 823.9 KB -

Airfoil tables [lift, drag and moment coefficients]; blade properties [radius, chord, twist] and airfoil coordinates; for the 193 cross-sectional segments of blade 022 of the southern wind turbine at the WINSENT test site; see the technical note (technical-note-3Dpolars_C.pdf) for more information

technical-note-3Dpolars_C.pdf

Jul 10, 2026 - Data for: Transforming Laser-Scanned 750 kW Turbine Surface Geometry Data into Smooth CAD for CFD Simulations

Adobe PDF - 1.2 MB -

This document describes the method used to obtain the airfoil tables (polars) for lift, drag, and moment using 3D URANS CFD on 193 segments for blade 022 within a one-third turbine model simulation.

technical-note-polar_twists_chord_Reynolds.pdf

Jul 10, 2026 - Data for: Transforming Laser-Scanned 750 kW Turbine Surface Geometry Data into Smooth CAD for CFD Simulations

Adobe PDF - 1.0 MB -

This document explains how to properly use the WINSENT airfoil aerodynamic tables (polars), with an emphasis on the twist, chord and Reynolds number distributions of each polar set. A method is also given to adjust the polars to a different twist and chord distribution, or to compare polar sets generated with different distributions.

glxiv2_single_node_fv_pid_tts_cpu_vs_gpu.csv

Jun 1, 2026 - GALÆXI v2.0: Performance

Comma Separated Values - 253 B -

glxiv2_single_node_power_to_solution_lumi_mn5.csv

Jun 1, 2026 - GALÆXI v2.0: Performance

Comma Separated Values - 155 B -

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