درباره ما
NASA-TN-D-1620
Effect of cross-section shape on the aerodynamic characteristics of bodies at mach numbers from 2.50 to 4.63
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:32:52Z | |
| date available | 2017-09-04T16:32:52Z | |
| date copyright | 01/01/1963 | |
| date issued | 1963 | |
| identifier other | USTKAEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/96325 | |
| description abstract | Effect of cross-section shape on aerodynamic characteristics of bodies at mach 2.50 to 4.63 - fuselage design | |
| language | English | |
| title | NASA-TN-D-1620 | num |
| title | Effect of cross-section shape on the aerodynamic characteristics of bodies at mach numbers from 2.50 to 4.63 | en |
| type | standard | |
| page | 31 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1963 | |
| contenttype | fulltext | |
| subject keywords | AERODYNAMIC | |
| subject keywords | CHARACTERISTICS | |
| subject keywords | FUSELAGE | |
| subject keywords | FUSELAGES | |
| subject keywords | MACH | |
| subject keywords | NUMBER | |
| subject keywords | SHAPES |
