1. If you were going to design an airspeed system with no errors, what would it

Question

1. If you were going to design an airspeed system with no errors, what would it look like? How would you eliminate the errors?

2. Compare and contrast the methods of measuring aerodynamic forces in a wind tunnel to that of an airplane in flight.

3. Compare and contrast an aircraft having a high aspect ratio wing to an aircraft that has a low aspect wing. What are the operational requirements that drive these designs? All things being equal, which aircraft will--in principle--have longer endurance and why? Which aircraft will lose more energy in flight under elevated G and why?

Explanation / Answer

1)

The ideal airspeed system can displays a airspeed is correct

socmany advanced technologies are used to find the aircraft speed

one of that is

using Pitot tubes given different types of airspeed of an aircraft incorrctly that cannot be

known sometimes by the staff of an aircraft.

So using GPS can find an airspeed is correct that using the accurate mechanical instruments such as the Pitot

tube.

So the old and new technologies are used then this will increase the safety of the aircraft..

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