Townend ring

A Townend ring is a narrow-chord cowling ring fitted around the cylinders of an aircraft radial engine to reduce drag and improve cooling.

Polish sports plane PZL Ł.2 with a Townend ring

Development

The Townend ring was the invention of Dr. Hubert Townend of the British National Physical Laboratory[1] in 1929. Patents were supported by Boulton & Paul Ltd in 1929.[2] In the United States it was often called a "drag ring". It caused a reduction in the drag of radial engines and was widely used in high-speed designs of 1930-1935 before the long-chord NACA cowling came into general use. Despite suggestions of it exploiting the Meredith effect, low airspeeds, low temperature differences and small mass flows make that unlikely,[3] particularly when combined with the lack of flow control as the air exits the cowling.[4] Although superior to earlier cowlings, and uncowled engines in terms of drag and cooling, above 217 kn (402 km/h; 250 mph) the NACA cowling was more efficient and soon replaced it in general use.[5]

A Luftwaffe Ju 52/3m being serviced in Crete in 1943: Note the narrow-chord Townend ring on the central engine and the deeper-chord NACA cowlings on the wing engines.

Examples of aircraft with Townend rings include the Boeing P-26 Peashooter, the Vickers Wellesley, the Fokker D.XVI and the centre engine on the Junkers Ju 52/3m.[lower-roman 1]

Notes

  1. The wing engines of the Ju52 had longer NACA cowlings, but the centre engine only had space for the shorter Townend ring.

References

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