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Stall strips

From Wikipedia, the free encyclopedia
Aerodynamic device
One of a pair of stall strips installed on an American Aviation AA-1 Yankee during manufacture

Astall strip is a small component fixed to theleading edge of thewing of anairplane to modify its aerodynamic characteristics.[1] These stall strips may be necessary for the airplane to comply withtype certification requirements.

A stall strip typically consists of a small piece of material, usually aluminium, triangular in cross section and often 6-12 inches (15–30 cm) in length. It isriveted orbonded to the wing’s leading edge. Some airplanes have one stall strip on each wing. Some airplanes have only one stall strip on one wing.

Operation

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TheCL-215 has a stall strip on the right wing only

A stall strip initiatesflow separation on a region of the upper surface of the wing during flight at highangle of attack. This is typically to avoid a tendency tospin following astall, or to improve the controllability of the airplane as it approaches the stall. A stall strip may be intended to alter the wing’s stall characteristics and ensure that thewing root stalls before thewing tips.[1]

In some cases, such as theAmerican Aviation AA-1 Yankee, both wings are designed to incorporate stall strips. In the case of the AA-1 the left and right wings were identical, interchangeable and built on a single wing jig, thus the more traditional use ofwashout in the wing design was not possible.[2]

Stall strips are usually factory-installed but, on rarer occasions, may be an after-market modification.

See also

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Wikimedia Commons has media related toStall strips.

References

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  1. ^abCrane, Dale:Dictionary of Aeronautical Terms, third edition, page 487. Aviation Supplies & Academics, 1997.ISBN 1-56027-287-2
  2. ^AviationConsumer (n.d.)."AGAC AA-1". Archived fromthe original on 2007-10-10. Retrieved2007-11-03.

External links

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