Bow shock (aerodynamics)

A bow shock, also called a detached shock or bowed normal shock, is a curved propagating disturbance wave characterized by an abrupt, nearly discontinuous, change in pressure, temperature, and density. It occurs when a supersonic flow encounters a body, around which the necessary deviation angle of the flow is higher than the maximum achievable deviation angle for an attached oblique shock.

Source: Wikipedia — Bow shock (aerodynamics) (CC BY-SA 4.0)

Bow shock (aerodynamics)

A bow shock, also called a detached shock or bowed normal shock, is a curved propagating disturbance wave characterized by an abrupt, nearly discontinuous, change in pressure, temperature, and density. It occurs when a supersonic flow encounters a body, around which the necessary deviation angle of the flow is higher than the maximum achievable deviation angle for an attached oblique shock.

Source: Wikipedia "Bow shock (aerodynamics)" · CC BY-SA 4.0

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