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Comparison between experimental and predicted downwash at a Mach number of 0.25 behind a wing-body combination having a triangular wing of aspect ratio of 2.0
| Content Provider | University of North Texas |
|---|---|
| Author | Sorensen, Norman E. Hopkins, Edward J. |
| Organization | Ames Aeronautical Laboratory (U.S.) |
| Description | A study to evaluate a method for predicting the downwash in a transverse plane behind a wing-body combination throughout a range of angles of attack. The wing-body combination had a ratio of maximum body diameter to wing span of 0.259, a triangular wing with an aspect ratio of 2.0, and a body of revolution with a fineness ratio of 12.5. Results regarding span loading, downwash, and vortex cores are provided. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc55958 |
| Language | English |
| Publisher Date | 2018-04-18 |
| Access Restriction | Open |
| Subject Keyword | wing-body combinations downwash aerodynamics |
| Content Type | Text |
| Resource Type | Report |