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Dynamic Stability Investigation of Two Right Circular Cylinders in Axial Free Flight at Mach Numbers From 0.4 to 1.7 Fineness-Ratio- 2.56 Cylinder and Fineness-Ratio-4.0 Cylinder With Flared Afterbody
| Content Provider | University of North Texas |
|---|---|
| Author | McFall, John C. Jr. |
| Organization | Langley Aeronautical Laboratory |
| Description | Memorandum presenting two right circular cylinders tested in axial free flight over a Mach number range of 0.4 to 1.7 by using the rocket-boosted-model technique. Results regarding time history, basic data cross plots, center of pressure, and drag are provided. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc53066 |
| Language | English |
| Publisher Date | 2018-12-19 |
| Access Restriction | Open |
| Subject Keyword | circular cylinders dynamic stability |
| Content Type | Text |
| Resource Type | Report |