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Aerodynamics of slender bodies at Mach number of 3.12 and Reynolds numbers from 2 x 10(exp 6) to 15 x 10(exp 6) 5: aerodynamic load distributions for a series of four boattailed bodies
| Content Provider | University of North Texas |
|---|---|
| Author | Moskowitz, Barry Jack, John R. |
| Organization | Lewis Flight Propulsion Laboratory |
| Description | Pressure distributions for a series of four boattailed bodies of revolution were obtained and compared with theory for a Mach number of 3.12, a Reynolds number range of 2 x 10 to 6th power to 14 x 10 to the 6th power, and angles of attack from zero to 9 degrees. Second-order theory adequately predicted the pressure distribution for regions free of the effects of cross-flow separation. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc60316 |
| Language | English |
| Publisher Date | 2018-07-05 |
| Access Restriction | Open |
| Subject Keyword | load distributions aerodynamics bodies of revolution |
| Content Type | Text |
| Resource Type | Report |