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NACA-TN-1428
Notes and tables for use in the analysis of supersonic flow
Year: 1947
Abstract: This paper is a compilation of formulas, tables, and curves that has been found to be very useful in the analysis of supersonic wind-tunnel data. The information has been compiled by members of the Ames 1- by 3-foot supersonic wind-tunnel section with the specific needs of supersonic wind-tunnel operation in mind.
With one exception, all tables and curves contained herein have been computed for the value of y = 1.400. The one exception is the curves showing the characteristics of cones in supersonic flow. These curves were taken directly from the data of references 1 and 2 wherein a value of y = 1.405 was used in the calculations.
With one exception, all tables and curves contained herein have been computed for the value of y = 1.400. The one exception is the curves showing the characteristics of cones in supersonic flow. These curves were taken directly from the data of references 1 and 2 wherein a value of y = 1.405 was used in the calculations.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:14:52Z | |
| date available | 2017-09-04T15:14:52Z | |
| date copyright | 01/01/1947 | |
| date issued | 1947 | |
| identifier other | MEPTYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/13749 | |
| description abstract | This paper is a compilation of formulas, tables, and curves that has been found to be very useful in the analysis of supersonic wind-tunnel data. The information has been compiled by members of the Ames 1- by 3-foot supersonic wind-tunnel section with the specific needs of supersonic wind-tunnel operation in mind. With one exception, all tables and curves contained herein have been computed for the value of y = 1.400. The one exception is the curves showing the characteristics of cones in supersonic flow. These curves were taken directly from the data of references 1 and 2 wherein a value of y = 1.405 was used in the calculations. | |
| language | English | |
| title | NACA-TN-1428 | num |
| title | Notes and tables for use in the analysis of supersonic flow | en |
| type | standard | |
| page | 86 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1947 | |
| contenttype | fulltext |