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FORWARD-SWEPT WINGS
Forward-swept wing looks really unusual. The better-known design is the Russian experimental fighter, the Sukhoi Su-47 Berkut. With the tips located forward of the point where the wings are connected to the fuselage, the plane almost looks as if it is flying backwards. Negative sweep (sweepfarward) has following advantages:
- It decreases induced drag as the airflow moves from the wing tips towards fuselage
- As a result ii increases lift-to-drag ratio and take off and landings characteristics
- Increases controllability
The main disadvantage is that the forward-swept wing is exposed to a torsion of wing. This phenomenon is also known as divergence – when the lift force on forward-swept wing twist the tip upwards. As a result it can lead to destruction. Thus the construction of the wing has to be strict enough to withstand these forces. Constructors also faced with aerodynamic shakings caused by reverse airflow on the wing which encounter the airflow from the fuselage. In addition to the mentioned above its important to highlight that this kind of wing is not good for high supersonic speed. The solution of these problems were not found so whole experiments were closed.
28 sty 2021 21:38
Poprawki · 3
1
FORWARD-SWEPT WINGS Forward-swept wing looks really unusual. The better-known
design is the Russian experimental fighter, the Sukhoi Su-47 Berkut. With the
tips located forward of the point where the wings are connected to the fuselage,
the plane almost looks as if it is flying backwards. Negative sweep
(sweepfarward) has the following advantages: - It decreases induced drag as the
airflow moves from the wing tips towards fuselage - As a result ii increases
lift-to-drag ratio and take off and landings characteristics - Increases
controllability The main disadvantage is that the forward-swept wing is exposed
to a torsion of wing. This phenomenon is also known as divergence – when the
lift force on forward-swept wing twist the tip upwards. As a result it can lead
to destruction. Thus the construction of the wing has to be strict enough to
withstand these forces. Constructors also faced with aerodynamic shakings caused
by reverse airflow on the wing which encounter the airflow from the fuselage. In
addition to the mentioned above its important to highlight that this kind of
wing is not good for high supersonic speed. The solutions to these problems were
not found so further experiments were ended.
29 stycznia 2021
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Oksana
Znajomość języków
angielski, rosyjski
Język do nauczenia się
angielski
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