1
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NAVY AVIATION Questions and Answers
(100% Correct Answers) Already Graded
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Wings [ Ans: ] The primary airfoils of the plane
Airfoil [ Ans: ] Anything designed to produce lift when it moves
through the air
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Cantilever Wing [ Ans: ] Has sufficient internal support structures
to keep it steady in its location
Semi-Cantilever Wing [ Ans: ] Requires additional external
support structures
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Flaps [ Ans: ] Run from the fuselage to the middle of the wing
Ailerons [ Ans: ] Run from the middle of the wing to the tip
Wingspan [ Ans: ] The distance from one wingtip to the other
Chord [ Ans: ] The distance from the leading edge to the trailing
edge is called the chord, which runs through the wing from
leading edge to trailing edge, it divides the wing into upper and
lower surfaces.
Mean Camber Line [ Ans: ] Runs along the inside of the wing,
such that the parts of the wing above and below it are equal in
thickness.
Camber [ Ans: ] The curvature of the airfoil: if an airfoil is heavily
curved, it has a high camber. The thickness of a wing is meaured
at its greatest point.
Planform [ Ans: ] The shape of the wings when viewed from
overhead
Dihedral Angle [ Ans: ] When the wings are not attached parallel
to the horizontal plane, the angle they make with the horizontal
plane
, 2
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Positive Dihedral Wing Angle [ Ans: ] Keeps the plane stable
when it rolls, as it will encourage the plane to return to its original
position
Straight Wings [ Ans: ] Are rectangular, rounded, or tapered.
They are commonly found on sailplanes, gliders, and other low-
speed aircraft
Swept Wing [ Ans: ] Provides better handling at high speeds, but
makes the plane slightly less stable at low speeds. Since most
modern aircraft are designed to operate at high speeds, this is the
most commonly used wing style
Delta Wing [ Ans: ] Is triangular, so that the leading edge of the
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wing has a high sweep angle while the trailing edge is mostly, if
not completely, straight. Enables the plane to travel but also
requires very high takeoff and landing speeds. Many of the earliest
supersonic aircraft used the wing shape, as did space shuttles
Guru01 - Stuvia
Fuselage [ Ans: ] The main body of the airplane,the basic
features are the cockpit, cabin, cargo area, and attachment
points for external components, like the wings and landing gear
Stringer [ Ans: ] A support structure that runs the length of the
fuselage
Former [ Ans: ] A support structure that runs perpendicular of the
fuselage
Tail Assembly (Empennage) [ Ans: ] Includes the vertical and
horizontal stabilizers, elevators, rudders, and trim tabs
Stabilizers [ Ans: ] Fixed surfaces that extend from the back end
of the fuselage
Elevators [ Ans: ] Positioned along the trailing edges of the
horizontal stabilizers; the pilot can move them to raise or lower the
nose of the plane
Rudders [ Ans: ] Connected to the trailing edge of the vertical
stabilizer, and are used to move the nose of the plane to the left
or right, typically in combination with the ailerons
For Expert help and assignment solutions, +254707240657
NAVY AVIATION Questions and Answers
(100% Correct Answers) Already Graded
A+
Wings [ Ans: ] The primary airfoils of the plane
Airfoil [ Ans: ] Anything designed to produce lift when it moves
through the air
© 2025 Assignment Expert
Cantilever Wing [ Ans: ] Has sufficient internal support structures
to keep it steady in its location
Semi-Cantilever Wing [ Ans: ] Requires additional external
support structures
Guru01 - Stuvia
Flaps [ Ans: ] Run from the fuselage to the middle of the wing
Ailerons [ Ans: ] Run from the middle of the wing to the tip
Wingspan [ Ans: ] The distance from one wingtip to the other
Chord [ Ans: ] The distance from the leading edge to the trailing
edge is called the chord, which runs through the wing from
leading edge to trailing edge, it divides the wing into upper and
lower surfaces.
Mean Camber Line [ Ans: ] Runs along the inside of the wing,
such that the parts of the wing above and below it are equal in
thickness.
Camber [ Ans: ] The curvature of the airfoil: if an airfoil is heavily
curved, it has a high camber. The thickness of a wing is meaured
at its greatest point.
Planform [ Ans: ] The shape of the wings when viewed from
overhead
Dihedral Angle [ Ans: ] When the wings are not attached parallel
to the horizontal plane, the angle they make with the horizontal
plane
, 2
For Expert help and assignment solutions, +254707240657
Positive Dihedral Wing Angle [ Ans: ] Keeps the plane stable
when it rolls, as it will encourage the plane to return to its original
position
Straight Wings [ Ans: ] Are rectangular, rounded, or tapered.
They are commonly found on sailplanes, gliders, and other low-
speed aircraft
Swept Wing [ Ans: ] Provides better handling at high speeds, but
makes the plane slightly less stable at low speeds. Since most
modern aircraft are designed to operate at high speeds, this is the
most commonly used wing style
Delta Wing [ Ans: ] Is triangular, so that the leading edge of the
© 2025 Assignment Expert
wing has a high sweep angle while the trailing edge is mostly, if
not completely, straight. Enables the plane to travel but also
requires very high takeoff and landing speeds. Many of the earliest
supersonic aircraft used the wing shape, as did space shuttles
Guru01 - Stuvia
Fuselage [ Ans: ] The main body of the airplane,the basic
features are the cockpit, cabin, cargo area, and attachment
points for external components, like the wings and landing gear
Stringer [ Ans: ] A support structure that runs the length of the
fuselage
Former [ Ans: ] A support structure that runs perpendicular of the
fuselage
Tail Assembly (Empennage) [ Ans: ] Includes the vertical and
horizontal stabilizers, elevators, rudders, and trim tabs
Stabilizers [ Ans: ] Fixed surfaces that extend from the back end
of the fuselage
Elevators [ Ans: ] Positioned along the trailing edges of the
horizontal stabilizers; the pilot can move them to raise or lower the
nose of the plane
Rudders [ Ans: ] Connected to the trailing edge of the vertical
stabilizer, and are used to move the nose of the plane to the left
or right, typically in combination with the ailerons
