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However, full supersonic flow over the vehicle will not develop until well past Mach 1.0.
This shock appears when supersonic flow in a pipe is decelerated.
However, in a supersonic flow, the pressure disturbance cannot propagate upstream.
In supersonic flows, expansion is achieved through an expansion fan.
Supernovae explosions are accompanied by supersonic flows and shock waves.
The shock wave is one of several different ways in which a gas in a supersonic flow can be compressed.
Subsonic and supersonic flow react differently to changes in cross sectional area.
A Ludwieg tube is a cheap and efficient way of producing supersonic flow.
Laminar supersonic flow was achieved in an experimental plane in the 1960's.
The Mach number is approximately one with combined subsonic and supersonic flow regions.
However, as its name implies, a scramjet combustor must address these challenges in a supersonic flow environment.
Thus the matter initially slows down, typically through a shock transition, and then accelerates again to become a supersonic flow.
A Ludwieg tube is a wind tunnel that produces supersonic flow for short periods of time.
Years of research and experience with the unusual conditions of supersonic flow have led to some interesting conclusions about airfoil design.
The paper concerned supersonic flow only.
Metal pressure chambers were used to store high-pressure air which was then accelerated through a nozzle designed to provide supersonic flow.
As an engineer, he was always focussed on applied research, such as gas dynamics in supersonic flows.
The major difficulty with the acoustic analogy, however, is that the sound source is not compact in supersonic flow.
Solar wind, a supersonic flow of electrified gases, carries with it the interplanetary magnetic field.
Conversely, the Mach number of a supersonic flow will decrease until the flow is choked.
It will occur when a supersonic flow encounters a corner that effectively turns the flow into itself and compresses.
Lighthill's early work included two dimensional aerofoil theory, and supersonic flow around solids of revolution.
Shocks are irreversible occurrence in supersonic flows (i.e. the entropy increases).
Supersonic flow can decelerate back to subsonic only in a normal shock; this typically happens before the trailing edge.
Wave drag is the simplest and most important component of the drag in supersonic flow flight regions.