Published June 8, 2020
| Version public
Book Section - Chapter
Progress on Experimental and Computational Investigation of Juncture Flows
Creators
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1.
Boeing (United States)
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2.
California Institute of Technology
Abstract
This paper describes a set of measurements taken at the Caltech Lucas Wind Tunnel, along with Computational Fluid Dynamic analyses, on a wing-body configuration. The configuration is designed to produce regions of separation in the juncture where the wing meets the body. Detailed near- and off-body stereo PIV measurements in the juncture flow are compared with predictions from computational methods based on the Reynolds Average Navier Stokes formulation. The results from the experimental measurements will become part of a database of high fidelity measurements, to be used for calibration of turbulence models and validation of emerging computational techniques.
Additional Information
© 2020 AIAA. Published Online: 8 Jun 2020.Additional details
Identifiers
- Eprint ID
- 103797
- Resolver ID
- CaltechAUTHORS:20200609-125716906
Dates
- Created
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2020-06-09Created from EPrint's datestamp field
- Updated
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2023-03-14Created from EPrint's last_modified field
Caltech Custom Metadata
- Caltech groups
- GALCIT
- Other Numbering System Name
- AIAA Paper
- Other Numbering System Identifier
- 2020-2734