The Airplane Flashcards
Definition of aeroplane/airplane
A power-driven heavier-than-air aircraft deriving its lift in flight from aerodynamic reactions on surfaces that remain fixed under given conditions of flight
Ways to classify fixed wing airplane
Position of wings (high/low), number of engines (single/multi), or undercarriage configuration (type of landing gear, retractable/conventional)
Essential parts of airplane
Fuselage, wings/lifting surfaces, empennage/canard, propulsion system (with/without propellers, engine(s)), undercarriage or landing gear
Airframe
All essential parts of airplane without propulsion system
Truss types
N Girder or Warren Truss
Longerons
3, 4, or more long tubes running lengthways, principle members and braced to form the frames
Monocoque
Skin/shell made to resist all of the loads, with no stiffening members used
Semi-monocoque
Some of loads and structure provided by stiffeners
5 systems of wing construction
- Metal frame, metal covered (Main strength in covering/skin)
- Metal frame, metal covered (main strength in frame)
- Metal frame, fabric covered
- Composite
- Wooden frame, fabric or plywood covered
Spars
Beams running from wing root to wing tip, carries most of load. Stiffens wing against torsion or twisting. Monospar found in certain modern airplanes with laminar flow airfoil wing design.
Ribs
Runs from leading to trailing edge. Cambered to form airfoil section. False/nose ribs sometimes made, attaching leading edge to main spar to strengthen leading edge.
Compression struts
Steel tubes intended to take compression loads. Spaced at regular intervals between front and rear spars.
Cantilever wings
Wings with no external bracing. Spars must be made strong enough to carry the load into the fuselage internally with no assistance.
Transmission of Loads -Internally
Load on wing comes first on skin. Then transmitted to the ribs, then to spars, then to fuselage.
Transmission of Loads -Externally
Externally braced wing. Part of load is taken by bracing struts or flying or landing wires, then transmitted to fuselage.