Aircraft Design Flashcards
What are the five major stresses to which all aircraft are subjected?
Tension, Compression, Torsion, Shear, and Bending
What type of stress is created when an object is twisted in opposite directions from each end?
Torsion
The three types of fuselage construction:
Truss Type, Monocoque, Semi-Monocoque
Numbered in inches from a reference or zero point known as a datum, these are used to locate specific places on an aircraft along a line parallel to the longitudinal axis.
Fuselage Stations
The two types of wing design for modern aircraft:
Cantilever, Semi-Cantilever
This type of wing requires no external bracing:
Cantilever
The primary load carrying member that runs parallel to the lateral axis in each wing of an aircraft:
Wing Spar
Wing ribs that are considered a part of the primary structure of the wing:
Compression Ribs
Wing ribs that are not considered a part of the primary structure of the wing:
Former Ribs
Nacelles or pods are streamlined enclosures used on multi-engine aircraft primarily to house ___ and ___ .
Engines and Landing Gear
These are detachable, permanently formed skins designed to fit over an engine to streamline airflow and aid in cooling the engine:
Cowlings
The name for the tail section of an airplane:
Empennage
The type of aircraft construction where all of the stress is carried in the strength of the skin:
Monocoque
The type of construction where all of the stress is carried in a rigid framework:
Truss-Type
The type of construction where all of the stress is carried in some combination of the skin and frame:
Semi-Monocoque