standard atmosphere वाक्य
उदाहरण वाक्य
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- This disparity is not a significant departure from accuracy, and USSA1976 uses this value of " R " * for all the calculations of the standard atmosphere.
- Airspeed indicators are calibrated on the assumption that they are operating at sea level in the International Standard Atmosphere where the air density is 1.225 kg / m 3.
- The temperature of the air varies with altitude, giving the following variations in the speed of sound using the standard atmosphere-" actual conditions may vary ".
- Once above the transition altitude, the altimeter is set to the international standard atmosphere ( ISA ) pressure at MSL which is 1013.25 hPa or 29.92 inHg.
- The pressure altitude system in an approved recorder has the same function as a barograph and must be calibrated to the ICAO ISA ( International Civil Aviation Organisation International Standard Atmosphere ).
- The IAS is not the actual speed through the air even when the aircraft is at sea level under International Standard Atmosphere conditions ( 15 �C, 1013 CAS ( Calibrated Airspeed ).
- "' Density altitude "'is the altitude relative to the standard atmosphere conditions ( air density would be equal to the indicated air density at the place of observation.
- Note also that, in a standard atmosphere, most oils begin to burn well below their boiling points . & mdash; Lomn 15 : 49, 24 February 2008 ( UTC)
- From current EASA definitions : Indicated airspeed means the speed of an aircraft as shown on its pitot static airspeed indicator calibrated to reflect standard atmosphere adiabatic compressible flow at sea level uncorrected for airspeed system errors.
- ICAO defines an International Standard Atmosphere ( also known as ICAO Standard Atmosphere ), a model of the standard variation of pressure, temperature, density, and viscosity with altitude in the Earth's atmosphere.
- ICAO defines an International Standard Atmosphere ( also known as ICAO Standard Atmosphere ), a model of the standard variation of pressure, temperature, density, and viscosity with altitude in the Earth's atmosphere.
- When flying at sea level under International Standard Atmosphere conditions ( 15 �C, 1013 hPa, 0 % humidity ) calibrated airspeed is the same as equivalent airspeed ( EAS ) and true airspeed ( TAS ).
- The nominal net thrust quoted for a jet engine usually refers to the Sea Level Static ( SLS ) condition, either for the International Standard Atmosphere ( ISA ) or a hot day condition ( e . g.
- Because the temperature of the atmosphere generally decreases with altitude ( until the tropopause ), the speed of sound also decreases with altitude . ( See the International Standard Atmosphere for more on temperature as a function of altitude .)
- The ICAO defines the International Standard Atmosphere ( also known as ICAO Standard Atmosphere ), which is the model of the standard variation of pressure, temperature, density, and viscosity with elevation / altitude in the Earth's atmosphere.
- The ICAO defines the International Standard Atmosphere ( also known as ICAO Standard Atmosphere ), which is the model of the standard variation of pressure, temperature, density, and viscosity with elevation / altitude in the Earth's atmosphere.
- For instance, precise measurements show that the boiling point of VSMOW water under one standard atmosphere of pressure is actually 373.1339 K ( 99.9839 �C ) when adhering " strictly " to the two-point definition of thermodynamic temperature.
- I wanted to add a second converted unit; the article previously had " . . . between 5 and 10 standard atmospheres ( 500 and 1, 000 kPa ) ", using the markup " convert | 5 | and | 10 | atm | sigfig = 1 ".
- In contrast the LM-105 designer Lutz M�ller originally calculated an optimistic G1 BC of H " 0.93 and a supersonic range of H " at a muzzle velocity of under International Standard Atmosphere sea level conditions ( air density ? = 1.225 kg / m 3 ).
- Though the M76 fires its bullets at a relatively modest muzzle velocity, the 8?7mm IS cartridge loaded with aerodynamically efficient military sS ball bullets still offers a supersonic reach of H " under ICAO Standard Atmosphere conditions at sea level ( air density ? = 1.225 kg / m?).
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