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Next: Upstream Mach number, M1, Up: Oblique Shock Previous: Oblique Shock Index Solution of Mach AngleOblique shock, if orientated to a coordinate perpendicular and parallel shock plane is like a normal shock. Thus, the relationship between the properties can be determined by using the normal components or by utilizing the normal shock table developed earlier. One has to be careful to use the normal components of the Mach numbers. The stagnation temperature contains the total velocity.
Again, the normal shock is a one-dimensional problem,
thus, only one parameter is required (to
solve the problem).
Oblique shock is a two-dimensional problem and
two properties must be provided so a solution can be found.
Probably, the most useful properties
are upstream Mach number,
Subsections
Next: Upstream Mach number, M1, Up: Oblique Shock Previous: Oblique Shock 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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and the deflection angle,
which create a somewhat complicated
mathematical procedure, and this will be discussed later.
Other combinations of properties provide a relatively simple
mathematical treatment, and the solutions of selected pairs and
selected relationships will be presented.