Tab10 - Shock

Normal and Oblique shockwave calculations are presented

Both upstream values are derived from the altitude and flight stream conditions.

Click the Calc button to calculate the Normal shock relations in the upper frame. Downstream values are presented.

Within the lower frame enter a ramp angle (degrees) and choose between a weak or strong solution.
Click the Calc button and the values will be shown.
The maximum ramp angle is displayed, values larger than this cannot be entered into the combo box.