Mach Angle Formula:
From: | To: |
The Mach angle (μ) is the angle formed between the direction of motion of a supersonic object and the Mach wave (shock wave) it creates. It occurs when an object moves faster than the speed of sound in that medium.
The calculator uses the Mach angle formula:
Where:
Explanation: The Mach angle decreases as the Mach number increases, meaning faster objects produce narrower shock wave cones.
Details: Mach angle calculation is crucial in aerodynamics for designing supersonic aircraft, analyzing shock waves, and understanding sonic boom patterns. It helps engineers optimize aircraft shapes for reduced drag and better performance at supersonic speeds.
Tips: Enter speed in m/s and speed of sound in m/s. Both values must be positive. Note that Mach angle is only defined for supersonic flows (Mach number ≥ 1).
Q1: What is the physical significance of Mach angle?
A: The Mach angle represents the half-angle of the Mach cone, which is the boundary between disturbed and undisturbed regions in a supersonic flow field.
Q2: Why is Mach angle undefined for subsonic flow?
A: For subsonic speeds (M < 1), the argument of the arcsine function becomes greater than 1, which is mathematically undefined since sine values range from -1 to 1.
Q3: How does temperature affect Mach angle calculations?
A: Temperature affects the speed of sound (which increases with temperature), thereby affecting the Mach number and consequently the Mach angle for a given speed.
Q4: What are typical Mach angle values for supersonic aircraft?
A: For commercial supersonic aircraft like Concorde (Mach 2), the Mach angle is about 30°. For hypersonic vehicles (Mach 5+), the angle is less than 12°.
Q5: Can Mach angle be measured experimentally?
A: Yes, Mach angle can be visualized using schlieren photography or shadowgraph techniques in wind tunnels, and measured from the angle of shock waves in flow visualization studies.