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NACA-TN-3583
Charts of boundary-layer mass flow and momentum for inlet performance analysis mach number range, 0.2 to 5.0
Year: 1955
Abstract: Mass flow and momentum for various fractions of a turbulent boundary layer are presented in chart form for a range of velocity profiles and for Mach numbers from 0.2 to 5.0. These charts are intended to assist the analyst and designer of boundary,layer removal systems. Application of the charts to inlets of arbitrary shape and to the determination of the pressure recovery of rectangular, normal-shock inlets immersed in boundary layer is described.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:10:08Z | |
| date available | 2017-09-04T18:10:08Z | |
| date copyright | 01/01/1955 | |
| date issued | 1955 | |
| identifier other | GWNUYDAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/193172 | |
| description abstract | Mass flow and momentum for various fractions of a turbulent boundary layer are presented in chart form for a range of velocity profiles and for Mach numbers from 0.2 to 5.0. These charts are intended to assist the analyst and designer of boundary,layer removal systems. Application of the charts to inlets of arbitrary shape and to the determination of the pressure recovery of rectangular, normal-shock inlets immersed in boundary layer is described. | |
| language | English | |
| title | NACA-TN-3583 | num |
| title | Charts of boundary-layer mass flow and momentum for inlet performance analysis mach number range, 0.2 to 5.0 | en |
| type | standard | |
| page | 27 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1955 | |
| contenttype | fulltext |