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NACA-TR-1135
Equations, tables, and charts for compressible flow
Year: 1953
Abstract: This report, which is a revision and extension of NACA-TN-1428, presents a compilation of equations, tables, and charts useful in the analysis of high-speed flow of a compressible fluid. The equations provide relations for continuous one-dimensional flow, normal and oblique shock waves, and Prandtl-Meyer expansions for both perfect and imperfect gases. The tables present useful dimensionless ratios for continuous one-dimensional flow and for normal shock waves as functions of Mach number for air considered as a perfect gas. One series of charts presents the characteristics of the flow of air (considered a perfect gas) for oblique shock waves and for cones in a supersonic air stream. A second series shows the effects of caloric imperfections on continuous one-dimensional flow and on the flow through normal and oblique shock waves. (author)
Subject: AIR
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:12:43Z | |
| date available | 2017-09-04T15:12:43Z | |
| date copyright | 01/01/1953 | |
| date issued | 1953 | |
| identifier other | LYDZYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/11266 | |
| description abstract | This report, which is a revision and extension of NACA-TN-1428, presents a compilation of equations, tables, and charts useful in the analysis of high-speed flow of a compressible fluid. The equations provide relations for continuous one-dimensional flow, normal and oblique shock waves, and Prandtl-Meyer expansions for both perfect and imperfect gases. The tables present useful dimensionless ratios for continuous one-dimensional flow and for normal shock waves as functions of Mach number for air considered as a perfect gas. One series of charts presents the characteristics of the flow of air (considered a perfect gas) for oblique shock waves and for cones in a supersonic air stream. A second series shows the effects of caloric imperfections on continuous one-dimensional flow and on the flow through normal and oblique shock waves. (author) | |
| language | English | |
| title | NACA-TR-1135 | num |
| title | Equations, tables, and charts for compressible flow | en |
| type | standard | |
| page | 70 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1953 | |
| contenttype | fulltext | |
| subject keywords | AIR | |
| subject keywords | CHARTS | |
| subject keywords | COMPRESSIBLE | |
| subject keywords | DATA | |
| subject keywords | DIMENSIONAL | |
| subject keywords | EQUATIONS | |
| subject keywords | EXPANSION | |
| subject keywords | FLOW | |
| subject keywords | GAS | |
| subject keywords | GRAPHS | |
| subject keywords | MACH | |
| subject keywords | MEYER | |
| subject keywords | NORMAL | |
| subject keywords | NUMBER | |
| subject keywords | OBLIQUE | |
| subject keywords | ONE | |
| subject keywords | PRANDTL | |
| subject keywords | RATIOS | |
| subject keywords | SHOCK | |
| subject keywords | SUBSONIC | |
| subject keywords | SUPERSONIC | |
| subject keywords | TABLES | |
| subject keywords | WAVES |