Brainstorm all possible terms related to the topic
Before you read the text name the main functions of the wing, try to describe wing structure. Share your ideas with your group mates.
Reading
Read the text and write a brief heading for each paragraph.
Read the text and write out the underlined words. Try to guess their meaning from the context. Compare your notes with your partners.
Wing
A. The main lifting surfaces of every airplane are wings. The wings are light structures which extend out on each side of the body. Their function is to push downward on the air as the machine moves through it. This push or lift of the wings is the secret of the support of the airplane in the air.
B. The wing is divided into three sections: a wing root, an inter-mediate section and a wing tip. The front edge of the wing is called the leading edge and the rear one is called the trailing edge. There are some movable parts on the trailing edge of the wing. These are ailerons, flaps and trimmer tabs.
C. The primary function of the wing is to produce lift (lifting force) for flying. The secondary function is to house many vital parts of the aircraft, such as fuel tanks, control mechanism and very often the engines and landing gear bay are arranged in the wing structure.
D. The distance from the wing tip on one side to the wing tip on the other side is called the span and the distance from the leading edge of the wing to the trailing edge is the chord.
E. The shape of the wing is of great importance for an aircraft. There are different configurations of the wing. There are rectangular and elliptical wings, wings of trapezoidal form, straight, sweptback and sweptforward wings. There is also a delta wing form.
F. The wing structure consists of longitudinal structural members - spars, stringers and beams and of transverse elements — ribs. The wing structure is covered with skin (or covering). According to the position in which the wing of a monoplane is fixed in relation to the fuselage the aircraft is called a low-wing monoplane, a mid-wing monoplane and a high-wing monoplane.
G. The aerodynamic loads on the wing produce bending, shear and torsion. A typical construction of a wing must resist these loads and usually consists of a thin sheet metal shell of airfoil shape, reinforced within by spanwise stiffeners and transverse ribs. Every component of an airplane must be so designed that it could carry its intended function.
H. Light weight is very important in an airplane structure because every pound of structural weight replaces a pound of payload. The wing structure is no exception in this respect. The stressed skin type of construction was adopted because it can be made light.
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Comprehension Check
Define the main idea of paragraph H. Find the supporting details that help to develop the main idea.
Complete the sentences with the best options.
1. There are some movable parts on the ______ of the wing.
a) leading edge b) trailing edge c) centre-section
2. The ______ structural members of the wing are spars, stringers and beams.
a) transverse b) covering c) longitudinal
3. The _______ the wing produce bending, shear and torsion.
a) weight of b) aerodynamic loads on c) structure of
4. Every pound of wing structural weight replaces a pound of _____ .
a) payload b) power c) lifting force
5. The distance between wing tips is called the _____.
a) chord b) beam c) span
Match the terms with their definitions.
1. In this type of construction the skin a. span
of the aircraft carries structural loads.
2. This component of the airplane b. skin
produces lifting force for flying.
3. They are the longitudinal members c. stressed skin
of the wing structure.
4. The distance between the d. chord
wing tips.
5. It covers the wing structure. e. wing
6. It is a transverse element of f. spar, stringer and beam
the wing structure.
7. Distance from the leading to g. rib
the trailing edge of the wing.
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