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Vortilon

From Wikipedia, the free encyclopedia
Aerodynamic device
Vortilons can be seen projecting from underneath the center leading edge of the wings of thisHawker 850XP

Vortilons are fixedaerodynamic devices on aircraft wings used to improve handling at low speeds.[1][2]

The vortilon was invented[3] by aerodynamicists working atDouglas Aircraft who had previously developed the engine pylons for theDouglas DC-8. The original pylons which wrapped around the leading edge of the wing had to be cut back to reduce excessive cruise drag.[4] Wind tunnel testing of the next Douglas commercial aircraft, theDouglas DC-9 which had no under-wing engines, showed a cutback engine pylon would be beneficial to wing lift and upwash at the tail at the low speed stall. The pylon was reduced in size and became the vortilon (VORTex-generating-pYLON).[5]

Vortilons consist of one or more flat plates attached to the underside of thewing near its leading edge, aligned with the flight direction.[6] When the speed is reduced and the aircraft approachesstall, the local flow at the leading edge is diverted outwards; this spanwise component of velocity around the vortilon creates avortex streamed around the top surface, which energises theboundary layer.[6] A more turbulent boundary layer, in turn, delays the local flow separation.

A view of three vortilons on the wing of a Cozy MKIV aircraft

Vortilons are often used to improve low-speedaileron performance,[1][7] thereby increasing resistance tospin. They can be used as an alternative towing fences, which also restrict airflow along the span of the wing.[1] Vortilons only stream vortices at highangles of attack[8] and produce less drag at higher speeds than wing fences.[9] Pylons used to mountjet engines under the wing produce a similar effect.[10]

The occurrence of span-wise flow at high angles of attack, such as observed onswept wings, is an essential requirement for vortilons to become effective. According toBurt Rutan, vortilons installed on straight wings would not have any effect.[11]

Vortilons were first introduced with theMcDonnell Douglas DC-9 to achieve a strong nose down pitching moment just beyond the normal stall and their influence ceased to have any effect beyond 30 degrees angle of attack.[10][12] They have been used on subsequent aircraft, including:


See also

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References

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  1. ^abcd"Unicom".Flying: 75. July 2002. Retrieved2011-10-07.
  2. ^Houghton, Edward Lewis; Carpenter, Peter William (2003).Aerodynamics for engineering students (5th ed.). Oxford: Butterworth-Heinemann. pp. 514.ISBN 0750651113.OCLC 50441321.
  3. ^"Stall control device for swept wings".
  4. ^https://www.scribd.com/document/50976964/Applied-aerodynamics-at-the-Douglas-Aircraft-Company, Fig.23
  5. ^https://arc.aiaa.org/doi/abs/10.2514/3.43770, p.Fig 13
  6. ^abRaymer, Daniel P. (1999). "8.2 Aerodynamic Considerations in Configuration Layout".Aircraft Design: A Conceptual Approach (3rd ed.). Reston, Virginia: American Institute of Aeronautics and Astronautics. p. 183.ISBN 1-56347-281-3.
  7. ^abMcClellan, J. Mac (November 2002)."Hawker 800XP".Flying: 75. Retrieved2011-10-07.
  8. ^Barnard, R.H.; Philpott, D.R. (2010). "Boundary layer and stalling problems on swept wings".Aircraft Flight (4th ed.). Harlow, England: Prentice Hall. p. 75.ISBN 978-0-273-73098-9.
  9. ^abMcClellan, J. Mac (February 1993)."BAE 1000 Lifts Hawker Name to New Heights".Flying: 88. Retrieved2011-10-07.
  10. ^ab"The DC-9 and the Deep Stall".Flight International: 442. 25 March 1965. Retrieved2011-10-07.
  11. ^Vortilons for Variezes,The canard pusher, n°42, October 1984
  12. ^Shevell, Richard S.; Schaufele, Roger D. (November–December 1966). "Aerodynamic Design Features of the DC-9".Journal of Aircraft.3 (6):515–523.doi:10.2514/3.43770.
  13. ^abSmith, Steve."Resources for learning about vortilons". NASA Quest. Archived fromthe original on 2010-11-11. Retrieved2011-10-07.
  14. ^https://archive.org/details/DTIC_ADA247719 8-4
  15. ^https://www.nasa.gov/centers/dryden/pdf/88410main_H-1957V1.pdf,p.87[dead link]

External links

[edit]
  • Media related toVortilon at Wikimedia Commons
  • Wing Vortex Devices from Aerospaceweb.org explains vortilons and other vortex-generating wing appliances
Aircraft components andsystems
Airframe structure
Flight controls
Aerodynamic andhigh-lift
devices
Avionic andflight
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