From Wikipedia, the free encyclopedia
Rear edge of an aerodynamic surface
For trailing edge in electronics, the back edge of a digital signal, see
Signal edge
.
Cross section of an aerodynamic surface with the trailing edge emphasised
An
American Aviation AA-1 Yankee
being refuelled. Its wing trailing edge can be seen with
aileron
(deployed downwards) and
flap
.
The
trailing edge
of an aerodynamic surface such as a
wing
is its rear edge, where the airflow separated by the
leading edge
meets.
[1]
Essential
flight control surfaces
are attached here to control the direction of the departing air flow, and exert a controlling force on the aircraft.
[2]
Such control surfaces include
ailerons
on the wings for roll control,
elevators
on the
tailplane
controlling
pitch
, and the
rudder
on the
fin
controlling
yaw
. Elevators and ailerons may be combined as
elevons
on
tailless aircraft
.
The shape of the trailing edge is of prime importance in the aerodynamic function of any aerodynamic surface. A sharp trailing edge is always employed in an airfoil.
[3]
George Batchelor
has written about:
- “ ... the remarkable controlling influence exerted by the sharp trailing edge of an aerofoil on the
circulation
.”
[4]
Extensions
[
edit
]
Other sharp-edged surfaces that are attached to the trailing edges of wings or control surfaces include:
Other equipment that may be attached to the trailing edges of wings include:
Trailing edge shape
[
edit
]
The trailing edge is where the upper and lower surfaces of a wing meet. They may meet at a finite angle. Alternatively, if the trailing edge angle is zero it is described as a
cusped
trailing edge.
[5]
References
[
edit
]
- ^
Crane, Dale:
Dictionary of Aeronautical Terms, third edition
, page 521. Aviation Supplies & Academics, 1997.
ISBN
1-56027-287-2
- ^
Wragg, David W. (1973).
A Dictionary of Aviation
(first ed.). Osprey. p. 262.
ISBN
9780850451634
.
- ^
“It had been known from the very beginning of flight that wings with a sharp trailing edge must be used in order to obtain a well-defined lift.”
von Mises, Richard
(1945),
Theory of Flight
, Section VIII.2, p.179, Dover Publications Inc. ISBN 0-486-60541-8
- ^
Batchelor, G. K. (1967),
An Introduction to Fluid Dynamics
, p.438, Cambridge University Press.
- ^
Anderson, John D. (2017).
Fundamentals of aerodynamics
. United States: McGraw-Hill Education. pp. 332?333.
ISBN
978-0-07-339810-5
.