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Next: Introduction to Prandtl-Meyer Function Up: Introduction Previous: Introduction Index Introduction to Oblique ShockA normal shock occurs when there is a disturbance downstream which imposes a boundary condition on the flow in which the fluid/gas can react only by a sharp change in the flow direction. As it may be recalled, normal shock occurs when a wall is straight/flat (
)
as shown in Figure (13.1)
which occurs when somewhere downstream a
disturbance13.2 appears.
When the deflection angle is increased,
the gas flow must match the boundary conditions.
This matching can occur only when there is a discontinuity in the flow field.
Thus, the direction of the flow is changed by a shock wave with an angle
to the flow.
This shock is commonly referred to as the oblique shock.
Alternatively, as discussed in
Chapter (1)13.3 the flow behaves as it does in
a hyperbolic field.
In such a case, the flow field is governed by a hyperbolic equation
which deals with the case when information (like boundary
conditions) reaches from
downstream only if they are within the range of influence.
For information such as the disturbance (boundary
condition) to reach deep into the flow from the side requires time.
During this time, the flow moves
downstream and creates an angle.
Next: Introduction to Prandtl-Meyer Function Up: Introduction Previous: Introduction Index Created by:Genick Bar-Meir, Ph.D. On: 2007-11-21 If you want the whole book or parts in pdf or other formats, then click here. You also can get the best and the largest gas dynamics tables in the world. About Potto Project
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