answersLogoWhite

0


Best Answer

Applying a load simultaneously, to the point where the aircraft cannot support itself.

User Avatar

Wiki User

11y ago
This answer is:
User Avatar

Add your answer:

Earn +20 pts
Q: What is shock loading in an aircraft?
Write your answer...
Submit
Still have questions?
magnify glass
imp
Related questions

How many feet should you be in when unloading and loading a parked aircraft?

If your unloading an aircraft, you need to be as close as possible.


What is shock loading in waste water?

When YOU are GOOD at something NEVER do it for FREE...


What is an airplane bay?

On a military transport aircraft it is the loading bay in the tail of the aircraft. on a passenger jet it is the cargo hatch on the rear side.


What is in SIC 3537?

Establishments manufacturing aircraft loading hoists are classified in SIC 3537


What is the speed of an aircraft when a conical shock wave is generated by a supersonic aircraft?

Generally speaking, a conical shock wave indicates a disturbance(in this case an aircraft) in the air travelling at a speed greater than that of the sound. But this only happens under ideal conditions. Real aircraft have very complex shapes and some part of the aircraft may experience shock wave earlier than the rest (over the bubble canopy or over the wing), so you usually don't get to find a perfect conical shock wave forming around an aircraft in real life.


What is wing loading of an aircraft?

Wing Loading is the details of the distribution of pressure on an aircraft wing. An aircraft flys by producing Lift by its wings. This lift force depends on the shape of the wing that produces high pressure on the bottom of the wing and low pressure on the top. The center of the lift is usually at the 1/4 chord or 25% of the width of the wing as measure from the leading edge. The Wing Loading can be designed to produce different Lift and ensure the aircraft will be easy to trim for level flight.


What is operating line?

Aircraft line operations refers to all of the various services performed on aircraft. This includes fueling, towing, deicing, loading & unloading and other services aircraft need between flights.


What is the difference between shock loading and dynamic loading of cranes?

A dynamic load arises from the acceleration or deceleration of a "static" load (mass). A shock load occurs when this acceleration or deceleration is very large and the the time frame is very short.


When considering cargo for selection on a specific airframe what publications should you use as reference?

When considering cargo for selection on a specific airframe, you should consult the aircraft's Weight and Balance Manual, Aircraft Flight Manual, and any specific cargo loading procedures provided by the aircraft manufacturer. These publications will provide you with important information on weight limitations, cargo compartment configurations, and loading restrictions specific to the aircraft.


Which produce a narrower conical shock wave- a slower or faster supersonic aircraft?

Faster


Air force driving regulations in aircrat parking area?

15 mph on the flightline. Slower if you are close to the aircraft. You need preplaced chocks if you are moving up to an aircraft for loading or unloading.


What is wing loading?

Simply put, wing loading is a calculation derived by dividing the weight of the aircraft by the area of the wing. It is used in aircraft design to determine a number of predicted performance characteristics such as take off speeds, climb ability, turn performance, etc. Generally, the lower the wing loading, the better the overall performance. However, there are some instances in which high wing loading produces more desirable performance characteristics for specific applications, such as military tactical maneuvering. The F-104 is a good example of the application of high wing loading.