Transonic flow is air flowing around an object at a speed that generates regions of both subsonic and supersonic airflow around that object. The exact range of speeds depends on the object's critical
Aerodynamic condensation evidences of supersonic expansion fans around a transonic F/A-18
Shock waves may appear as weak optical disturbances above airliners with supercritical wings
Adolf Busemann was a German aerospace engineer and influential Nazi-era pioneer in aerodynamics, specialising in supersonic airflows. He introduced the concept of swept wings and, after emigrating in