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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) 4: aerodynamic characteristics of series of four bodies having near-parabolic noses and cylindrical afterbodies
| Content Provider | University of North Texas |
|---|---|
| Author | Jack, John R. Moskowitz, Barry |
| Organization | Lewis Flight Propulsion Laboratory |
| Description | Pressure distributions and forces for a series of four bodies of revolution having nose-fineness ratios varying from 4 to 10 have been obtained and compared with theory for a Mach number of 3.12, a Reynolds number range of 2x10(sup)6 to 14x10(sup)6, and angles of attack from zero to 9 degrees. In general, a comparison of the experimental data with a second-order theory showed good agreement for the range of variables investigated. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc59119 |
| Language | English |
| Publisher Date | 2018-07-05 |
| Access Restriction | Open |
| Subject Keyword | pressure distributions bodies of revolution aerodynamics |
| Content Type | Text |
| Resource Type | Report |
