Example 14.3 A supersonic two-dimensional inlet is to be operate at M 3.0. Two possibilities will be considered, as shown in Figure 14.8. In one, the compression and slowing down of the flow take place through one normal shock; in the other, a wedge-shaped diffuser, the deceleration occurs through two weak oblique shocks, followed by a normal shock. The wedge turning angles are each 8°. Compare the loss in stagnation pressure for the two cases shown.

Example 14.3 A supersonic two-dimensional inlet is to be operate at M 3.0. Two possibilities will be considered, as shown in Figure 14.8. In one, the compression and slowing down of the flow take place through one normal shock; in the other, a wedge-shaped diffuser, the deceleration occurs through two weak oblique shocks, followed by a normal shock. The wedge turning angles are each 8°. Compare the loss in stagnation pressure for the two cases shown.

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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