Resultant force on aircraft door

In summary, the question asks for the resultant force on a door with an area of 2m^2 situated in an aircraft with a maintained cabin pressure of 100kPa while flying at an altitude with an air pressure of 28kPa. The solution involves finding the difference in pressure and calculating the resultant force on the door, which is ultimately balanced by reaction forces from the hinges.
  • #1
Andy21
20
0

Homework Statement


The air pressure at the altitude an aircraft is flying at is 28kPa. If the pressure inside the cabin is maintained at 100kPa, what is the resultant force on a door of area 2m^2 in the side of the aircraft?

Homework Equations





The Attempt at a Solution



I am not sure whether the answer is 0N because the door must be stationary and therefore no resultant force must be acting on it or do you have to work out the pressures exerted on the door from outside and inside the aircraft and then subtract the smaller of the forces.
 
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  • #2
Yes, your looking for the resultant force from the pressure difference over that area. The reason the door doesn't move is because there is reaction forces applied by the hinges..so the true net force on the door is zero.
 
  • #3
thanks for the help
 

Related to Resultant force on aircraft door

What is the resultant force on an aircraft door?

The resultant force on an aircraft door is the total force acting on the door, taking into account both magnitude and direction. It is the sum of all the forces acting on the door, including any external forces such as wind or gravity, as well as any internal forces from the aircraft structure.

How is the resultant force on an aircraft door calculated?

The resultant force on an aircraft door is calculated using vector addition. This involves adding together all the individual forces acting on the door, taking into account their direction and magnitude. The resulting vector represents the resultant force on the door.

What factors can affect the resultant force on an aircraft door?

The resultant force on an aircraft door can be affected by a variety of factors, including the speed and direction of the aircraft, the weight and distribution of the cargo and passengers, and the aerodynamic design of the aircraft. External factors such as wind and turbulence can also have an impact on the resultant force.

Why is it important to consider the resultant force on an aircraft door?

The resultant force on an aircraft door is an important consideration in aircraft design and operation. Too much force on the door can cause it to deform or even fail, compromising the safety of the aircraft and its passengers. Understanding and managing the resultant force is crucial for maintaining the structural integrity of the aircraft.

How can the resultant force on an aircraft door be managed?

The resultant force on an aircraft door can be managed through proper design and engineering. This includes considering the aerodynamics of the door and its surrounding structure, as well as implementing safety features such as reinforced hinges and latches. Additionally, pilots must be aware of external factors that can affect the resultant force and make adjustments to the aircraft's speed and direction as needed.

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