Measure shock angle from the incident flow to the shock front, and deflection towards it. The strong normal-compression ratio and continuity of tangential velocity give . Angle-addition identities reduce this to . The two title branches exist for and merge at . As , their formal limits are and . The weak-branch expansion requires ; at finite Mach number its true zero-deflection limit is the Mach angle.

Articles by others on the same topic (0)

There are currently no matching articles.