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Investigation of Two Bluff Shapes in Axial Free Flight Over a Mach Number Range From 0.35 and 2.15
| Content Provider | University of North Texas |
|---|---|
| Author | Coltrane, Lucille C. |
| Organization | Langley Aeronautical Laboratory |
| Description | Memorandum presenting a fineness-ratio-2.71 right circular cylinder and a fineness-ratio-4.0 circular cylinder with a rounded nose and a flared afterbody tested in free flight over a range of Mach and Reynolds numbers. Time histories, cross plots of force coefficients, rolling velocity, and longitudinal-force coefficient are presented for both cylinders. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc63741 |
| Language | English |
| Publisher Date | 2018-07-24 |
| Access Restriction | Open |
| Subject Keyword | circular cylinders aerodynamics |
| Content Type | Text |
| Resource Type | Report |