Formula Used:
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The Local Shock-detachment Distance is the distance of shock formation from the leading edge of a sphere cone body shape in supersonic flow. It represents the point where the shock wave detaches from the body surface.
The calculator uses the formula:
Where:
Explanation: This formula calculates the distance at which the shock wave detaches from the leading edge based on the body radius and flow Mach number.
Details: Accurate calculation of shock-detachment distance is crucial for aerodynamic design, understanding flow separation patterns, and predicting pressure distribution around sphere cone body shapes in supersonic flows.
Tips: Enter the radius in meters and Mach number. Both values must be positive numbers (radius > 0, Mach number > 0).
Q1: What factors affect shock-detachment distance?
A: The primary factors are the body radius and the flow Mach number. Higher Mach numbers generally result in smaller detachment distances.
Q2: How accurate is this formula?
A: This empirical formula provides reasonable estimates for sphere cone body shapes in typical supersonic flow conditions, but actual results may vary based on specific flow conditions and body geometry.
Q3: Can this formula be used for other body shapes?
A: This specific formula is designed for sphere cone body shapes. Other body shapes may require different formulas or computational methods.
Q4: What are typical values for shock-detachment distance?
A: The distance varies significantly with Mach number and body size, typically ranging from fractions of the radius to several times the radius.
Q5: How does temperature affect the calculation?
A: Temperature effects are indirectly accounted for through the Mach number, which depends on the local speed of sound that varies with temperature.