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NASA-TN-D-71
An approximate method for calculating surface pressures on curved profile blunt plates in hypersonic flow
Year: 1959
Abstract: The effects of profile curvature on the flow over blunt plates was investigated. A method of calculating surface pressures was developed which utilized a combination of viscous andinviscid hypersonic parameters. The method was assessed by comparison to experiment conducted in air and helium over a range of Mach numbers from 4 to 13.3 and leading-edge Reynolds numbers from 6,600 to 129,000 for elliptic and circular leading edges.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:44:58Z | |
| date available | 2017-09-04T15:44:58Z | |
| date copyright | 01/01/1959 | |
| date issued | 1959 | |
| identifier other | PQTKAEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/47434 | |
| description abstract | The effects of profile curvature on the flow over blunt plates was investigated. A method of calculating surface pressures was developed which utilized a combination of viscous andinviscid hypersonic parameters. The method was assessed by comparison to experiment conducted in air and helium over a range of Mach numbers from 4 to 13.3 and leading-edge Reynolds numbers from 6,600 to 129,000 for elliptic and circular leading edges. | |
| language | English | |
| title | NASA-TN-D-71 | num |
| title | An approximate method for calculating surface pressures on curved profile blunt plates in hypersonic flow | en |
| type | standard | |
| page | 28 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1959 | |
| contenttype | fulltext |