Mach Angle evaluator uses Mach Angle = asin(1/Mach Number) to evaluate the Mach Angle, Mach Angle formula is defined as the angle formed between the direction of a supersonic flow and the direction of the wavefront. It is crucial in understanding shock waves and their behavior in compressible flow scenarios. 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.