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NACA-TN-2200
A study of second-order supersonic-flow theory
Year: 1951
Abstract: An attempt is made to develop a second approximation to the solution of problems of supersonic flow which can be solved by existing first-order theory. The method of attack adopted is an iteration process using the linearized solution as the first step.
For plane flow it is found that a particular solution of the iteration equation can be written down at once in terms of the first-order solution. The second-order problem is thereby reduced to an equivalent first-order, problem and can be readily solved. At the surface of a single body, the solution reduces to the well-known result of Busemann. The plane case is considered in some detail insofar as it gives insight into the nature of the iteration process.
For plane flow it is found that a particular solution of the iteration equation can be written down at once in terms of the first-order solution. The second-order problem is thereby reduced to an equivalent first-order, problem and can be readily solved. At the surface of a single body, the solution reduces to the well-known result of Busemann. The plane case is considered in some detail insofar as it gives insight into the nature of the iteration process.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:48:52Z | |
| date available | 2017-09-04T18:48:52Z | |
| date copyright | 01/01/1951 | |
| date issued | 1951 | |
| identifier other | KQDUYDAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsessionid=3826AF679D40527318548F1EFDEC014A/handle/yse/230175 | |
| description abstract | An attempt is made to develop a second approximation to the solution of problems of supersonic flow which can be solved by existing first-order theory. The method of attack adopted is an iteration process using the linearized solution as the first step. For plane flow it is found that a particular solution of the iteration equation can be written down at once in terms of the first-order solution. The second-order problem is thereby reduced to an equivalent first-order, problem and can be readily solved. At the surface of a single body, the solution reduces to the well-known result of Busemann. The plane case is considered in some detail insofar as it gives insight into the nature of the iteration process. | |
| language | English | |
| title | NACA-TN-2200 | num |
| title | A study of second-order supersonic-flow theory | en |
| type | standard | |
| page | 74 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1951 | |
| contenttype | fulltext |