normal shock वाक्य
उदाहरण वाक्य
मोबाइल
- This region of supersonic acceleration is terminated by a normal shock wave.
- "Normal shocks " are a fundamental type of shock wave.
- Oblique shock waves are used predominantly in engineering applications when compared with normal shock waves.
- Normal shocks only happen when the flow is supersonic.
- This thin film of molecules act as normal shocks.
- Downstream of this normal shock the air is subsonic.
- The ratio of stagnation temperatures remains constant across a normal shock since the process is adiabatic.
- Interestingly, the intersection points occur at the given initial Mach number and its post-normal shock value.
- NASCAR's answer to the problem was to dictate that normal shocks would be run on each wheel.
- Normal shock waves can occur in two reference frames : the standing normal shock and the moving shock.
- Normal shock waves can occur in two reference frames : the standing normal shock and the moving shock.
- A detached normal shock wave forms just ahead of the intake lip and'shocks'the flow down to a subsonic velocity.
- The flow before a normal shock wave must be supersonic, and the flow after a normal shock must be subsonic.
- The flow before a normal shock wave must be supersonic, and the flow after a normal shock must be subsonic.
- A detached, strong normal shock appears directly in front of the inlet at supersonic flight speeds, which leads to poor pressure recovery.
- For supersonic flow, however, pitot pressure is the stagnation pressure of the flow behind the normal shock ahead of the pitot tube.
- When the compressed flow becomes parallel to the center line, a shock wave perpendicular to the flow forms, called a normal shock wave.
- Next, the equation below shows the relationship between the post normal shock temperature, T _ 2, and the upstream ambient temperature, T _ 1.
- This deceleration, which is produced by a normal shock, creates a total pressure loss which limits the upper operating point of a ramjet engine.
- Supersonic flow can decelerate back to subsonic only in a normal shock; this typically happens before the trailing edge . ( Fig . 1a)
- अधिक वाक्य: 1 2
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