normal shock उदाहरण वाक्य

उदाहरण वाक्य

1. Normal shock waves can occur in two reference frames : the standing normal shock and the moving shock.
2. A detached normal shock wave forms just ahead of the intake lip and'shocks'the flow down to a subsonic velocity.
3. The flow before a normal shock wave must be supersonic, and the flow after a normal shock must be subsonic.
4. The flow before a normal shock wave must be supersonic, and the flow after a normal shock must be subsonic.
5. A detached, strong normal shock appears directly in front of the inlet at supersonic flight speeds, which leads to poor pressure recovery.
6. For supersonic flow, however, pitot pressure is the stagnation pressure of the flow behind the normal shock ahead of the pitot tube.
7. When the compressed flow becomes parallel to the center line, a shock wave perpendicular to the flow forms, called a normal shock wave.
8. Next, the equation below shows the relationship between the post normal shock temperature, T _ 2, and the upstream ambient temperature, T _ 1.
9. This deceleration, which is produced by a normal shock, creates a total pressure loss which limits the upper operating point of a ramjet engine.
10. Supersonic flow can decelerate back to subsonic only in a normal shock; this typically happens before the trailing edge . ( Fig . 1a)