A normal shock at Mach 2.00, and what crosses it unchanged
The state in front of the shock and the state behind it. Every ratio was computed from the standard jump relations and then substituted back into mass, momentum and energy, which is an independent route — a mistyped exponent in the total-pressure expression cannot survive a momentum balance it never appeared in. The residuals are printed below because a check nobody can see is a check nobody can audit.
14 essays call
normal-shock. The drawing above is what it returns with no arguments at all; every
call below passes it something, because a placement that passes nothing draws whichever member
of the family the generator happens to default to rather than the one its essay argues about.
It is also the blast radius. Changing normal-shock changes every figure listed here
at once, and on this site it may change what they assert as well as what they show —
which is what has to be rebuilt and looked at before the change is believed.
Where it is called
What each of these essays asks for instead of the defaults is on the regime index, which reads the parameters back out of the finished figures rather than out of the placements.
- Energy instead of pressure Compressible flow
- What the airspeed indicator believes What is taught wrongly
- The shock in a river Fluids at work
- The jump the equations allow Compressible flow
- The pocket on top of the wing Regimes and numbers
- The only law that forbids it Compressible flow
- What a shock costs Compressible flow
- A shock that leans Compressible flow
- When the wedge is too blunt Compressible flow
- One diaphragm, every wave Compressible flow
- The bubble that hammers Fluids at work
- The wall that heats itself Compressible flow
- The viscosity nobody uses Viscosity
- A cone finishes its turn after the shock Compressible flow