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How does the temperature of the air change as you increase in altitude in the troposphere?
As you increase in altitude in the troposphere, the temperature usually decreases. This is because the air becomes less dense with higher altitude, leading to less heat retention and a decrease in temperature.
What does the temperature do as you increase in altitude?
Temperature decreases as altitude increases because there are less molecules in the atmosphere to hold in the heat.
Is it true that atmospheric pressure decreases with increased altitude?
Yes, it is true that atmospheric pressure decreases with increased altitude. This is because there is less air above pushing down on the air below as you go higher in the atmosphere. This is why it becomes harder to breathe at high altitudes due to the lower pressure.
As altitude increases in the Troposphere does the temperature increase?
No, as altitude increases in the Troposphere, the temperature generally decreases. This is because the Troposphere is the layer of the Earth's atmosphere where weather occurs, and the temperature decreases with altitude due to the decrease in air pressure and thinning of the air molecules that can store heat.
Does the temperature increase or decrease with altitude in the thermoshpere?
The temperature increases like the stratosphere
What is True airspeed indicator?
It's an airspeed indicator that compensates for outside temperature and barometric pressure at altitude.
What indicated airspeed should be selected for a particular altitude?
Basically, there are indicated, true and ground speeds. Indicated airspeed takes air pressure differences from a sensor, corrects for pressure altitude (altitude adjusted for barometric pressure) and for temperature to determine true airspeed (speed through the ocean of air). True airspeed is adjusted for winds to get ground speed. There are many factors to consider when selecting a particular air speed. For a particular airplane, fuel efficiency generally decreases with airspeed. Increased airspeed places more demands on piloting skills. If you know all the factors, you can determine the indicated of airspeed in the cockpit. Conversely, if the factors are known, ground speed can be determined from indicated airspeed. Winds aloft, which often change with altitude, are a bigger factor for small planes than for large commercial aircraft on a schedule. For fuel efficiency reasons, when experiencing a tailwind, use a lower indicated airspeed. Conversely, when in a headwind, use a higher airspeed. Either the benefits are greater or the penalty is not as severe when wind is considered. Look at it this way. You would like to stay in a tailwind to get that free push as long as possible, so, fly slower. Different airplanes have different fuel efficiency with airspeed characteristics so the optimum airspeed would vary with the airplane, the priorities of schedule, fuel efficiency and safety as well as weather conditions. Indicated airspeed decreases with altitude, so an altitude correction must be used to get the true airspeed as well as a temperature correction (it gets colder up there). They say speed is money. How fast do you want to go? So, it is a trade off among competing factors.
What is the difference between true airspeed and groundspeed?
Airspeed is speed with respect to the air, i.e. speed through the air. Groundspeed is speed with respect to the ground, i.e. speed over the ground. It's the vector sum of airspeed and windspeed.
What is rule of thumb that may be used to determine true air speed?
True airspeed (TAS) can be calculated by adjusting indicated airspeed (IAS) for nonstandard pressure and temperature conditions. A common rule of thumb is to add approximately 2% of the IAS per 1,000 feet of altitude to correct for the decrease in air density with altitude. This rule helps pilots estimate the TAS without needing to perform complex calculations in real-time during flight. However, for precise calculations, the pilot should refer to the aircraft's performance charts or use a flight computer to determine the TAS more accurately.
What is equivalent airspeed?
Equivalent airspeed is speed at sea level in which the incompressible dynamic pressure can be produces as if it were at true airspeed. Equivalent airspeed is used to predict aircraft handling.
How does airspeed indicator work?
The airspeed indicator operates based on the difference between the pressure of the pitot tube (ram air pressure) and the static port (ambient air pressure). As the aircraft moves through the air, the pressure difference changes, which is translated into an airspeed reading on the indicator. The indicator is calibrated to display the indicated airspeed, which may differ from the true airspeed due to factors like altitude and instrument errors.
What is the limitation of the airspeed indicator?
some V speeds are not indicated, It doesn't show true airspeed or ground speed.
Why as density altitude increase reduce speed of helicopter?
To compensate for the decreased air density the rotor blades need a greater angle of attack, pushing the retreating blade closer to stall(reducing the maximum airspeed)
What raises and lowers a plane during flight?
It depends on your airspeed. At normal cruise airspeed, an increase or decrease of engine thrust causes an aircraft to ascend or descend. At approach airspeed, a slower airspeed with flaps lowered, raising or lowering the elevators causes the aircraft to ascend or descend.
Temperature increase altitude increase?
No, it decreases.
What could describe an airplane's velocity?
The main two useful velocity measurements are... 1. KTAS- Knots (True Airspeed) 2. KIAS- Knots (Indicated Airspeed)
How do you calculate TAS from CAS andMN?
True airspeed (TAS) can be calculated from calibrated airspeed (CAS) by applying the compressibility correction factor based on altitude and temperature. The Mach number (MN) can be used to adjust the calculated TAS to account for the effects of speed of sound at the given conditions. TAS is typically calculated using the formulas provided in aviation manuals or with the help of specialized flight computers.
