Mach Angle evaluator uses Mach Angle = asin(1/Mach Number) to evaluate the Mach Angle, Mach Angle formula is defined as the angle between the direction of a supersonic flow and the direction of the wavefronts produced by that flow. It is crucial for understanding shock waves in aerospace applications. Mach Angle is denoted by μ symbol.
How to evaluate Mach Angle using this online evaluator? To use this online evaluator for Mach Angle, enter Mach Number (M) and hit the calculate button.