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NACA-TR-D-1374
The similarity rules for second-order subsonic and supersonic flow
Year: 1958
Abstract: The similarity rules for linearized compressible flow theory (Gothert's rule and its supersonic counterpart) are extended to second order. It is shown that any second-order subsonic flow can be related to "nearly incompressible" flow past the same body, which can be calculated by the Janzen-Rayleigh method.
Subject: BODIES OF REVOLUTION
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:48:13Z | |
| date available | 2017-09-04T17:48:13Z | |
| date copyright | 01/01/1958 | |
| date issued | 1958 | |
| identifier other | EQONEEAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std/handle/yse/171409 | |
| description abstract | The similarity rules for linearized compressible flow theory (Gothert's rule and its supersonic counterpart) are extended to second order. It is shown that any second-order subsonic flow can be related to "nearly incompressible" flow past the same body, which can be calculated by the Janzen-Rayleigh method. | |
| language | English | |
| title | NACA-TR-D-1374 | num |
| title | The similarity rules for second-order subsonic and supersonic flow | en |
| type | standard | |
| page | 8 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1958 | |
| contenttype | fulltext | |
| subject keywords | BODIES OF REVOLUTION | |
| subject keywords | COMPRESSIBLE FLOW | |
| subject keywords | CONES | |
| subject keywords | CYLINDRICAL BODIES | |
| subject keywords | FLOW THEORY | |
| subject keywords | SIMILITUDE LAW | |
| subject keywords | STEADY FLOW | |
| subject keywords | SUBSONIC FLOW | |
| subject keywords | SUPERSONIC FLOW | |
| subject keywords | THREE DIMENSIONAL BODIES |