| Download | - View final version: Rayleigh Line tabulation (PDF, 1.6 MiB)
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| DOI | Resolve DOI: https://doi.org/10.4224/40003789 |
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| Author | Search for: Cockshutt, E. P.1 |
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| Affiliation | - National Research Council Canada. National Aeronautical Establishment
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| Format | Text, Memorandum |
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| Physical description | 8 p. |
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| Abstract | Numerical Rayleigh Line data with ɤ= 1.3 are tabulated for the subsonic regime (M=0.00 to 1.00) for increments of Mach number of 0.01. A numerical example is included to illustrate the use of this table. |
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| Publication date | 1954-07-15 |
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| Publisher | National Research Council Canada |
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| Series | |
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| Language | English |
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| Peer reviewed | No |
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| Export citation | Export as RIS |
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| Report a correction | Report a correction (opens in a new tab) |
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| Record identifier | cf8aa2d8-3b09-448d-b40f-ab48b9d7b658 |
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| Record created | 2025-10-14 |
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| Record modified | 2025-11-03 |
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