한국   대만   중국   일본 
Trailing edge - Wikipedia Jump to content

Trailing edge

From Wikipedia, the free encyclopedia
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:

  • On control surfaces:
  • Other surfaces:

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 ]

  1. ^ Crane, Dale: Dictionary of Aeronautical Terms, third edition , page 521. Aviation Supplies & Academics, 1997. ISBN   1-56027-287-2
  2. ^ Wragg, David W. (1973). A Dictionary of Aviation (first ed.). Osprey. p. 262. ISBN   9780850451634 .
  3. ^ “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
  4. ^ Batchelor, G. K. (1967), An Introduction to Fluid Dynamics , p.438, Cambridge University Press.
  5. ^ Anderson, John D. (2017). Fundamentals of aerodynamics . United States: McGraw-Hill Education. pp. 332?333. ISBN   978-0-07-339810-5 .