For supersonic flow, however, pitot pressure is the stagnation pressure of the flow behind the normal shock ahead of the pitot tube.
32.
Supersonic flow can decelerate back to subsonic only in a normal shock; this typically happens before the trailing edge . ( Fig . 1a)
33.
These secondary shockwaves are caused by the air being forced to turn around these convex points, which generates a shock wave in supersonic flow.
34.
Maintaining combustion in the supersonic flow presents additional challenges, as the fuel must be injected, mixed, ignited, and burned within milliseconds.
35.
As p b is lowered below that needed to just choke the flow, a region of supersonic flow forms just downstream of the throat.
36.
There he worked with Professor Sydney Goldstein, a mathematician noted for his contribution to fluid dynamics, and wrote papers on supersonic flow and turbulence.
37.
The aerodynamic conditions required for flutter vary with the structure's external design and flexibility, but can range from very low velocities to supersonic flows.
38.
A supercritical airfoil has its maximum thickness close to the leading edge to have a lot of length to slowly shock the supersonic flow back to subsonic speeds.
39.
Perhaps the most recognizable supersonic aircraft, the SR-71, used a hydraulically actuated cone to reduce the speed of the supersonic flow through the aircraft inlet.
40.
Bill's earlier research into supersonic flow in Australia was ideal preparation for this work, and constituted invaluable expertise and management experience for the new tasks on Concorde.
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