11,694 research outputs found
tomrobin-teschner/softwareTesting: v.0.3.6
No full textA simple starter project for unit, integration and system testing purposes using the meson build system. An exemplary linear algebra library is developed to highlight how meson could be used in this environment
tomrobin-teschner/softwareTesting: v.0.3.7
No full textA simple starter project for unit, integration and system testing purposes using the meson build system. An exemplary linear algebra library is developed to highlight how meson could be used in this environment
Dataset DrivAer hp-F: Force Measurements at Various Rear Wing Angles of Attack
No full textDataset for the aerodynamic force measurements on the 35% scale DrivAer hp-F rear wing configuration using the moving ground facility in the 8x6 Wind Tunnel at Cranfield University. The dataset includes aerodynamic force coefficients results from the moving ground experiments on the DrivAer hp-F with rear wing angle of attack settings ranging from 0°-27.5°. The measurements have been conducted three times at each angle of attack setting for repeatability. In reference to the publication: Steven Rijns, Tom-Robin Teschner, Kim Blackburn, James Brighton; Effects of cornering conditions on the aerodynamic characteristics of a high-performance vehicle and its rear wing. Physics of Fluids 1 April 2024; 36 (4): 045119. https://doi.org/10.1063/5.0204204 CAD files for the DrivAer hp-F rear wing configuration are available at: Rijns, Steven; Teschner, Tom-Robin; Blackburn, Kim; Ramos Proenca, Anderson; Brighton, James (2024). DrivAer hp-F: Spoiler & Rear Wing Configurations Geometry Pack. Cranfield Online Research Data (CORD). Dataset. https://doi.org/10.17862/cranfield.rd.25715202
Dataset DrivAer hp-F: Force Measurements at Various Rear Wing Angles of Attack
No full textDataset for the aerodynamic force measurements on the 35% scale DrivAer hp-F rear wing configuration using the moving ground facility in the 8x6 Wind Tunnel at Cranfield University.
The dataset includes aerodynamic force coefficients results from the moving ground experiments on the DrivAer hp-F with rear wing angle of attack settings ranging from 0°-27.5°.
The measurements have been conducted three times at each angle of attack setting for repeatability.
In reference to the publication:
Steven Rijns, Tom-Robin Teschner, Kim Blackburn, James Brighton; Effects of cornering conditions on the aerodynamic characteristics of a high-performance vehicle and its rear wing. Physics of Fluids 1 April 2024; 36 (4): 045119. https://doi.org/10.1063/5.0204204
CAD files for the DrivAer hp-F rear wing configuration are available at:
Rijns, Steven; Teschner, Tom-Robin; Blackburn, Kim; Ramos Proenca, Anderson; Brighton, James (2024). DrivAer hp-F: Spoiler & Rear Wing Configurations Geometry Pack. Cranfield Online Research Data (CORD). Dataset. https://doi.org/10.17862/cranfield.rd.25715202
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Dataset DrivAer hp-F: Surface Pressure Measurements in Yaw Conditions
No full textDataset for the surface pressure measurements conducted on the 35% scale DrivAer hp-F model at various yaw angles in the 8x6 Wind Tunnel at Cranfield University.
The dataset includes the surface pressure coefficient results from measurements on the slant of the following vehicle configurations:
- DrivAer hp-F standard configuration (no spoiler or rear wing)
- DrivAer hp-F spoiler configuration
- DrivAer hp-F rear wing configuration
The measurements on the DrivAer hp-F rear wing configuration have been conducted three times for repeatability. The dataset also includes a log file of the data structure and wind tunnel conditions for each experiment.
In reference to the publication: Steven Rijns, Tom-Robin Teschner, Kim Blackburn, Anderson Ramos Proenca, James Brighton; Experimental and numerical investigation of the aerodynamic characteristics of high-performance vehicle configurations under yaw conditions. Physics of Fluids 1 April 2024; 36 (4): 045112. https://doi.org/10.1063/5.0196979
CAD files for the DrivAer hp-F configurations are available at: Rijns, Steven; Teschner, Tom-Robin; Blackburn, Kim; Ramos Proenca, Anderson; Brighton, James (2024). DrivAer hp-F: Spoiler & Rear Wing Configurations Geometry Pack. Cranfield Online Research Data (CORD). Dataset. https://doi.org/10.17862/cranfield.rd.25715202
Note: The updated datasets retain all original data while adding calibrated data to provide (new) users with an additional reference option
Data DrivAer hp-F: Spoiler & Rear Wing Configurations Geometry Pack
No full textCAD geometry files for the 35% scale high-performance DrivAer model (DrivAer hp-F). The dataset includes CAD files for the: - DrivAer hp-F vehicle body, equipped with a 41 mm front bumper splitter, a full set of large forebody strakes, and a 10° underbody multichannel diffuser. - Rear wing with a NACA 6412 profile, chord of 110 mm, and span of 420 mm. - Spoiler with a plate size of 350 x 80 mm at a 40° angle of attack - Wheels (stationary and rotating) In reference to the publications: Steven Rijns, Tom-Robin Teschner, Kim Blackburn, Anderson Ramos Proenca, James Brighton; Experimental and numerical investigation of the aerodynamic characteristics of high-performance vehicle configurations under yaw conditions. Physics of Fluids 1 April 2024; 36 (4): 045112. https://doi.org/10.1063/5.0196979 Steven Rijns, Tom-Robin Teschner, Kim Blackburn, James Brighton; Effects of cornering conditions on the aerodynamic characteristics of a high-performance vehicle and its rear wing. Physics of Fluids 1 April 2024; 36 (4): 045119. https://doi.org/10.1063/5.0204204 This geometry pack uses components from the original DrivAer hp-F: the CAD geometry pack collection: Soares, Renan francisco; Olives, Sergio Goñalons; Knowles, Andrew Paul; Garry, Kevin; Holt, Jenny (2018). DrivAer hp-F: the CAD geometry pack. Cranfield Online Research Data (CORD). Collection. https://doi.org/10.17862/cranfield.rd.c.396912
Dataset DrivAer hp-F: Wake Total Pressure Measurements in Yaw Conditions
No full textDataset for the wake total pressure measurements conducted on the 35% scale DrivAer hp-F model at various yaw angles in the 8x6 Wind Tunnel at Cranfield University. The measurements are performed on the DrivAer hp-F rear wing configuration with an angle of attack of 15°. The dataset includes the total pressure coefficient results from measurements on the P1, P2, and P3 wake planes, which are located 400 mm, 700 mm, and 1000 mm downstream of the vehicle model respectively. Additionally, the horizontal and vertical measurements positions (in mm) are provided for each wake plane. A horizontal sweep on the P3 wake plane has been conducted three times for repeatability.
In reference to the publication: Steven Rijns, Tom-Robin Teschner, Kim Blackburn, Anderson Ramos Proenca, James Brighton; Experimental and numerical investigation of the aerodynamic characteristics of high-performance vehicle configurations under yaw conditions. Physics of Fluids 1 April 2024; 36 (4): 045112. https://doi.org/10.1063/5.0196979
CAD files for the DrivAer hp-F rear wing configuration are available at: Rijns, Steven; Teschner, Tom-Robin; Blackburn, Kim; Ramos Proenca, Anderson; Brighton, James (2024). DrivAer hp-F: Spoiler & Rear Wing Configurations Geometry Pack. Cranfield Online Research Data (CORD). Dataset. https://doi.org/10.17862/cranfield.rd.25715202
Note: The updated dataset retains all original data while adding calibrated data to provide (new) users with an additional reference option
Dataset DrivAer hp-F: Force Measurements in Yaw Conditions
No full textDataset for the aerodynamic force measurements conducted on the 35% scale DrivAer hp-F model at various yaw angles in the 8x6 wind Tunnel at Cranfield University. The dataset includes aerodynamic force coefficients results from measurement on the following vehicle configurations: - DrivAer hp-F standard configuration (no spoiler or rear wing) - DrivAer hp-F spoiler configuration - DrivAer hp-F rear wing configuration The measurements on the DrivAer hp-F rear wing configuration have been conducted three times for repeability. In reference to the publication: Steven Rijns, Tom-Robin Teschner, Kim Blackburn, Anderson Ramos Proenca, James Brighton; Experimental and numerical investigation of the aerodynamic characteristics of high-performance vehicle configurations under yaw conditions. Physics of Fluids 1 April 2024; 36 (4): 045112. https://doi.org/10.1063/5.0196979 CAD files for the DrivAer hp-F configurations are available at: Rijns, Steven; Teschner, Tom-Robin; Blackburn, Kim; Ramos Proenca, Anderson; Brighton, James (2024). DrivAer hp-F: Spoiler & Rear Wing Configurations Geometry Pack. Cranfield Online Research Data (CORD). Dataset. https://doi.org/10.17862/cranfield.rd.2571520
DrivAer hp-F: Spoiler & Rear Wing Configurations Geometry Pack
No full text
CAD geometry files for the 35% scale high-performance DrivAer model (DrivAer hp-F).
The dataset includes CAD files for the:
- DrivAer hp-F vehicle body, equipped with a 41 mm front bumper splitter, a full set of large forebody strakes, and a 10° underbody multichannel diffuser.
- Rear wing with a NACA 6412 profile, chord of 110 mm, and span of 420 mm.
- Spoiler with a plate size of 350 x 80 mm at a 40° angle of attack
- Wheels (stationary and rotating)
In reference to the publications:
Steven Rijns, Tom-Robin Teschner, Kim Blackburn, Anderson Ramos Proenca, James Brighton; Experimental and numerical investigation of the aerodynamic characteristics of high-performance vehicle configurations under yaw conditions. Physics of Fluids 1 April 2024; 36 (4): 045112. https://doi.org/10.1063/5.0196979
Steven Rijns, Tom-Robin Teschner, Kim Blackburn, James Brighton; Effects of cornering conditions on the aerodynamic characteristics of a high-performance vehicle and its rear wing. Physics of Fluids 1 April 2024; 36 (4): 045119. https://doi.org/10.1063/5.0204204
This geometry pack uses components from the original DrivAer hp-F: the CAD geometry pack collection:
Soares, Renan francisco; Olives, Sergio Goñalons; Knowles, Andrew Paul; Garry, Kevin; Holt, Jenny (2018). DrivAer hp-F: the CAD geometry pack. Cranfield Online Research Data (CORD). Collection. https://doi.org/10.17862/cranfield.rd.c.3969120
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Dataset DrivAer hp-F: Surface Pressure Measurements in Yaw Conditions
No full textDataset for the surface pressure measurements conducted on the 35% scale DrivAer hp-F model at various yaw angles in the 8x6 Wind Tunnel at Cranfield University.
The dataset includes the surface pressure coefficient results from measurements on the slant of the following vehicle configurations:
- DrivAer hp-F standard configuration (no spoiler or rear wing)
- DrivAer hp-F spoiler configuration
- DrivAer hp-F rear wing configuration
The measurements on the DrivAer hp-F rear wing configuration have been conducted three times for repeatability.
The dataset also includes a log file of the data structure and wind tunnel conditions for each experiment.
In reference to the publication:
Steven Rijns, Tom-Robin Teschner, Kim Blackburn, Anderson Ramos Proenca, James Brighton; Experimental and numerical investigation of the aerodynamic characteristics of high-performance vehicle configurations under yaw conditions. Physics of Fluids 1 April 2024; 36 (4): 045112. https://doi.org/10.1063/5.0196979
CAD files for the DrivAer hp-F configurations are available at:
Rijns, Steven; Teschner, Tom-Robin; Blackburn, Kim; Ramos Proenca, Anderson; Brighton, James (2024). DrivAer hp-F: Spoiler & Rear Wing Configurations Geometry Pack. Cranfield Online Research Data (CORD). Dataset. https://doi.org/10.17862/cranfield.rd.25715202
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