Use LEFT and RIGHT arrow keys to navigate between flashcards;
Use UP and DOWN arrow keys to flip the card;
H to show hint;
A reads text to speech;
14 Cards in this Set
- Front
- Back
Divided into flight deck/control cabin and other compartments according to mission and design
|
Fuselage
|
|
Design where frame and skin combine to support loads and absorb stresses
|
Semi-Monocoque design
|
|
What are the structural members of the fuselage
|
Longerongs, Bulkheads, Rings and Formers, Stringers, Skin and Fairing
|
|
Which structural member is the longest and strongest and runs longitudinally (nose to tail)
|
The Longerons
|
|
How many Longerons are there normally on the fuselage
|
2 upper and 2 lower
|
|
Walls that separate fuselage into compartments and provide cross-sectional strength
|
Bulkheads
|
|
Provide shape and cross-sectional stength
|
Rings and Formers
|
|
Metal strips which run parallel to longerons, provide attaching points for skin and adds cross-sectional strength
|
Stringers
|
|
Covers, Streamlines, and Strengthens fuselage
|
Skin
|
|
Curved panel which streamlines surface areas where needed to reduce drag
|
Fairing
|
|
Provide access for inspection and maintenance
|
Access panels and doors
|
|
Provide lift and house fuel tanks
|
Wings
|
|
What wing design is internally braced to reduce drag
|
Cantilever
|
|
Extend from the wing root to tip; Longest and strongest members of the wing
|
Spars
|