• माख-शंकु • मैक शंकु | |
mach: मैक | |
cone: गजरौल गावदुम शंकु | |
mach cone मीनिंग इन हिंदी
mach cone उदाहरण वाक्य
उदाहरण वाक्य
अधिक: आगे- As the Mach number increases, so does the strength of the shock wave and the Mach cone becomes increasingly narrow.
- For instance, at Mach 1.3 the angle of the Mach cone formed off the body of the aircraft will be at about sin? = 1 / M ( ? is the sweep angle of the Mach cone)
- For instance, at Mach 1.3 the angle of the Mach cone formed off the body of the aircraft will be at about sin? = 1 / M ( ? is the sweep angle of the Mach cone)
- :: I think the " Mach cone " might be related to the Mach number, there a picture from Sound barrier which seems to fit .-- talk ) : 06 : 49, 12 July 2011 ( UTC)
- A more rational question is " do passengers on a supersonic jet hear engine noise " and the answer is, only if they are in the Mach cone behind the engine . moink 08 : 31, 16 June 2006 ( UTC)
- The PK-3 Plus experiment allows investigating a large variety of topics, for instance : the crystal structure, fluid-solid phase transitions, electrorheological fluids, wave propagation, the heartbeat instability, Mach cone formation and the speed of sound, and lane formation
- Because the different radial directions around the aircraft's direction of travel are equivalent ( given the " smooth flight " condition ), the shock wave forms a " Mach cone ", similar to a vapour cone, with the aircraft at its tip.
- For example, consider that at Mach 1.3 the angle of the Mach cone formed off the body of the aircraft will be at about ? = arcsin ( 1 / M ) = 50.3?( ? is the angle of the Mach cone, or simply Mach angle ).
- For example, consider that at Mach 1.3 the angle of the Mach cone formed off the body of the aircraft will be at about ? = arcsin ( 1 / M ) = 50.3?( ? is the angle of the Mach cone, or simply Mach angle ).
- When an aircraft exceeds Mach 1 ( i . e . the sound barrier ), a large pressure difference is created just in front of the aircraft . This abrupt pressure difference, called a shock wave, spreads backward and outward from the aircraft in a cone shape ( a so-called Mach cone ).