Normal Shock Wave Approximations for Flight at Hypersonic Mach Numbers
Normal shock pressure ratios in equilibrium air for Mach numbers up to 30 and altitudes to 300,000 feet are shown to be correlated by a simple power law which provides an accuracy of ±2%, thereby permitting direct calculation of corresponding enthalpy ratios accurate to ±1% without iteration; a slig...
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| Format: | Artigo |
| Sprache: | Inglês |
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MDPI AG
2026-01-01
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| Schriftenreihe: | Aerospace |
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| Online-Zugang: | https://www.mdpi.com/2226-4310/13/2/115 |
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