درباره ما
NACA-RM-E51H13
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) I - body of revolution with near-parabolic forebody and cylindrical afterbody
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:17:33Z | |
| date available | 2017-09-04T17:17:33Z | |
| date copyright | 01/01/1951 | |
| date issued | 1951 | |
| identifier other | ZIMCWDAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std/handle/yse/140894 | |
| description abstract | An experimental investigation of the aerodynamic characteristics of a slender, square-based body of revolution was conducted at a Mach number of 3.12 for angles of attack from 0 degree to 10 degrees and for Reynolds numbers from 2 x 10(exp 6) to 15 x 10(exp 6). Boundary-layer measurements at zero angle of attack are compared with several compressible flow formulating for predicting boundary-layer characteristics. Comparison of experimental pressure and force values with theoretical values showed good agreement for low angles of attack. The measured mean skin-friction coefficients agreed well with those predicted by Mangler's transformation for laminar flow over cones. | |
| language | English | |
| title | NACA-RM-E51H13 | num |
| title | 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) I - body of revolution with near-parabolic forebody and cylindrical afterbody | en |
| type | standard | |
| page | 48 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1951 | |
| contenttype | fulltext | |
| subject keywords | AERODYNAMIC | |
| subject keywords | BODIES | |
| subject keywords | FLOW | |
| subject keywords | LAMINAR | |
| subject keywords | LOADS | |
| subject keywords | SUPERSONIC | |
| subject keywords | TURBULENT |
