Mach Angle Formula:
Where:
θ: Mach cone angle (degrees)
M: Mach number (dimensionless)
From: | To: |
Definition: This calculator determines the angle of the shock wave (Mach cone) created by an object moving at supersonic speeds.
Purpose: It helps aeronautical engineers, physicists, and aviation enthusiasts understand shock wave behavior at different Mach numbers.
The calculator uses the formula:
Where:
Explanation: As an object moves faster than sound (M > 1), it creates a conical shock wave. The angle of this cone decreases as speed increases.
Details: Understanding Mach angles is crucial for aircraft design, sonic boom prediction, and analyzing supersonic flow patterns.
Tips: Enter the Mach number (must be ≥ 1). The calculator will show the corresponding Mach cone angle in degrees.
Q1: Why can't Mach number be less than 1?
A: Mach angles only exist for supersonic speeds (M ≥ 1). Below Mach 1, no shock wave forms.
Q2: What's a typical Mach angle for commercial jets?
A: Most jets fly subsonic (M < 1), but the Concorde flew at M≈2 (θ≈30°).
Q3: How does altitude affect Mach angle?
A: The angle depends only on Mach number, but sound speed (and thus true airspeed for a given M) changes with altitude.
Q4: What's the minimum possible Mach angle?
A: As M approaches infinity, θ approaches 0°. At M=1, θ=90°.
Q5: How is this related to sonic booms?
A: The Mach angle determines how "sharp" the shock wave is, affecting boom intensity on the ground.