WorksheetsAAP W11 - Aircraft Envelope and Loading
Total questions: 7
Worksheet time: 4mins
The upper speed limit of an aircraft is determined by:
aerodynamic stall performance
structural limitations and power/thrust available
cabin pressurization limits and power/thrust available
power/thrust available only
In steady, level cruise, the load n is:
0
1
need more information
-1
An aircraft in in a steady banked turn with a load factor n of 1.2. The roll angle is:
45 degrees
60 degrees
35.56 degrees
12.67 degrees
The boundary associated with permanent structural deformation on a V-n diagram is the.
ultimate load factor
limit load factor
To obtain the smallest possible turn radius in a banked level turn, we want:
the highest possible n and lowest possible V
the lowest possible n and lowest possible V
the lowest possible n and highest possible V
the highest possible n and highest possible V
The 'never exceed speed' is the speed at which the aircraft reaches aerodynamic stall.
true
false
Most aircraft maintain the cabin pressure equivalent to about ____ for good passenger comfort.
35,000ft
6,000ft
1,000ft
18,000ft
