The Airplane Flashcards

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1
Q

Definition of aeroplane/airplane

A

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

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2
Q

Ways to classify fixed wing airplane

A

Position of wings (high/low), number of engines (single/multi), or undercarriage configuration (type of landing gear, retractable/conventional)

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3
Q

Essential parts of airplane

A

Fuselage, wings/lifting surfaces, empennage/canard, propulsion system (with/without propellers, engine(s)), undercarriage or landing gear

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4
Q

Airframe

A

All essential parts of airplane without propulsion system

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5
Q

Truss types

A

N Girder or Warren Truss

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6
Q

Longerons

A

3, 4, or more long tubes running lengthways, principle members and braced to form the frames

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7
Q

Monocoque

A

Skin/shell made to resist all of the loads, with no stiffening members used

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8
Q

Semi-monocoque

A

Some of loads and structure provided by stiffeners

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9
Q

5 systems of wing construction

A
  1. Metal frame, metal covered (Main strength in covering/skin)
  2. Metal frame, metal covered (main strength in frame)
  3. Metal frame, fabric covered
  4. Composite
  5. Wooden frame, fabric or plywood covered
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10
Q

Spars

A

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.

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11
Q

Ribs

A

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.

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12
Q

Compression struts

A

Steel tubes intended to take compression loads. Spaced at regular intervals between front and rear spars.

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13
Q

Cantilever wings

A

Wings with no external bracing. Spars must be made strong enough to carry the load into the fuselage internally with no assistance.

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14
Q

Transmission of Loads -Internally

A

Load on wing comes first on skin. Then transmitted to the ribs, then to spars, then to fuselage.

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15
Q

Transmission of Loads -Externally

A

Externally braced wing. Part of load is taken by bracing struts or flying or landing wires, then transmitted to fuselage.

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16
Q

Ailerons

A

Surfaces, usually of airfoil section, hinged to the trailing edge of the wing towards each wing tip for lateral control. Usually hinged to rear spar.

17
Q

Flaps

A

Form part of wing structure. Usually hinged to rear spar.

18
Q

Wing Tip Bow

A

Generally a metal tube, curved to give the wing tip the particular shape required

19
Q

Wing Root

A

Section of wing nearest fuselage. For low wing, reinforced to allow passengers to walk on it.

20
Q

Wing Root Fittings

A

Fittings which attach the wing, or separate wing panels, to the fuselage

21
Q

Winglet

A

A small nearly vertical winglike surface attached to wing tip. Reduces induced drag

22
Q

Chord/ Mean Aerodynamic Chord (MAC)

A

Imaginary straight line joining leading and trailing edges of wing./Average chord of wing

23
Q

Span

A

Maximum distance from wing tip to wing tip of an airfoil, wing, or stabilizer.