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Oblique Shock Calculator
Turn angle from Mach number and shock angle
📖 Oblique Shock Calculator
For supersonic flow, tanθ = 2cotβ[(M₁²sin²β−1)/(M₁²(γ+cos2β)+2)]. Provide upstream Mach and shock angle β.
📊 Result
💡 Tips & Information
- Oblique Shock Calculator uses standard engineering formulas; always verify with project requirements.
- Keep units consistent across all inputs to avoid conversion errors.
- Field conditions, tolerances, and safety factors may require additional adjustments.