SABS-CFD-22: CFD and PIV Applications in Aviation |
Website | https://www.sares.org/sabs-cfd-2022 |
Submission link | https://easychair.org/conferences/?conf=sabs-cfd-2022 |
Abstract registration deadline | August 15, 2022 |
Submission deadline | August 30, 2022 |
To improve the overall performance of unmanned aerial vehicles (UAVs), the design should allow for the efficient use of energy, which can be translated into larger payloads and improved operational range. To improve UAV performance, these two factors motivate the quest for innovative propulsion architectures that demonstrate high synergy with the airframe and the remaining components and subsystems. These innovative propulsion architectures can assist in enhancing UAV performance. In this context, technologies such as dare distributed propulsion, thrust split, and boundary layer ingestion are examined comprehensively. CFD-based simulation tools have proven their ability to achieve ambitious performance goals.
Propulsion configuration for unmanned aerial vehicles (UAVs) requires the evaluation of a prototype configuration before the design of the airframe utilizing any propulsion system technique. The CFD solutions enable the aerodynamic performance to be evaluated prior to physical testing. On the other hand, PIV solutions enable the prototype to be tested in a physical environment, which is necessary before safety concerns can be authorized.
Unmanned aerial vehicles with fans or propellers for vertical takeoff and landing operations and wings that can move at higher speeds can deliver greater thrust or lift for a given diameter. However, these aerodynamic devices are susceptible to a wide range of atmospheric conditions. Using simulated environmental conditions, researchers can validate their theories using PIV. High-resolution PIV measurements provide accurate aerodynamic measurements that are a valid basis for later analytical and computational design investigations. PIV observations and computational predictions of mean flow near an aerodynamic device, such as a fan, propeller blade, or wing surface, are used to quantify aerodynamic movement performance.
Submission Guidelines
All papers must be original and not simultaneously submitted to another journal or conference. The following paper categories are welcome:
- Full papers describing CFD and PIV Applications in Aviation
- Full papers must be sent by the Springer Template can be found from this link
- https://drive.google.com/drive/folders/1-493DEecL_jbqCMfJQtRGYhSiR1EFk8Y?usp=sharing
- No Posters allowed
List of Topics
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Components for Flow Measurement Techniques
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Fluid, Correlation, and Other Flow Measurement Assessments
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Turbulence Models For Particle Image Velocimetry
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Software, Sector, Geometry In Particle Image Velocimetry
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Novel Propulsion Simulation Approaches
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CFD Examples to Design UAV Airframe
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Unmanned Aero Vehicle (UAV) Technologies
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New Generation Aero Vehicle Design Procedures
Committees
Program Committee
- Hikmet Karakoc
- Ozgur Colpan
- Alper Dalkiran
Organizing committee
- Hikmet Karakoc
- Ozgur Colpan
- Alper Dalkiran
Publication
SABS-CFD-22 chapters will be published in CFD and PIV Applications in Aviation Book by Springer
Contact
All questions about submissions should be emailed to sustainableaviationbook@gmail.com
Please do not hesitate to email the below email if you haven't get update from the above email adress
alperdalkiran@gmail.com