Clark Y is the name of a particular aerofoil profile, widely used in general purpose aircraft designs, and much studied in aerodynamics over the years. The profile was designed in 1922 by Virginius E. Clark. The airfoil has a thickness of 11.7 percent and is flat on the lower surface from 30 percent of chord back. The flat bottom simplifies angle measurements on propellers, and makes for easy construction of wings on a flat surface.
For many applications the Clark Y has been an adequate airfoil section; it gives reasonable overall performance in respect of its lift-to-drag ratio, and has gentle and relatively benign stall characteristics. But the flat lower surface is not optimal from an aerodynamic perspective, and it is rarely used in modern designs.
The Clark Y has found favour for the construction of model aircraft, thanks to the flight performance that the section offers at medium Reynolds number airflows. Applications on model aircraft is very wide, ranging from free-flight gliders through to multi-engined radio control scale models.
The Clark Y is appealing for its near-flat lower surface, which aids in the construction of wings on plans mounted on a flat construction board. Inexperienced modellers are more readily able to build model aircraft which provide a good flight performance with benign stalling characteristics.
Some of the better known aircraft that use the Clark Y and YH include:
- The Incomplete Guide to Airfoil Usage Retrieved 27 May 2013.
- Шавров В.Б. (1994) История конструкций самолетов в СССР 1938-1950 гг. (3 изд.). Машиностроение (Shavrov V.B. (1994) Istorija konstruktsij samoljotov v SSSR, 1938-1950 gg. (3rd ed.). Mashinostroenie. ISBN 5-217-00477-0) (History of aircraft design in USSR: 1938-1950)
- Lednicer, David, (15 September 2010), The Incomplete Guide to Airfoil Usage, retrieved 28 May 2013
- Piccirillo, Albert, "The Clark Y Airfoil - A Historical Retrospective," SAE/AIAA paper 2000-01-5517, presented at the World Aviation Congress & Exposition, October 10, 2000, San Diego, California.
- Martin Simons, Model Aeroplane Aerodynamics, Model & Allied Publications 1978. Chapter 7 - 9, Aerofoil Sections.
- (29 June 2005), From NASA to NASCAR, retrieved 29 April 2017