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Townend ring

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Title: Townend ring  
Author: World Heritage Encyclopedia
Language: English
Subject: Cowling, Aeronca L, Chyeranovskii BICh-14, Stampe et Vertongen SV.5 Tornado, Airspeed Envoy
Collection: Aircraft Propulsion Components
Publisher: World Heritage Encyclopedia

Townend ring

Polish sports plane PZL Ł.2 with a 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.


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. It was also said to generate forward thrust from the expansion of the air as it passed over the engine, adding 10 to 15 mph to the aircraft's top speed; but such an effect is physically implausible given the temperature differences and mass flows involved.[3]

Examples of aeroplanes with Townend rings were the Douglas O-38, Vickers Wellesley, the Westland Wallace and the Gloster Gauntlet. Early claims portrayed it as a superior design to the NACA cowling, but later comparisons proved aircraft performance worse when using a Townend ring at airspeeds above 250 mph.[4]


  1. ^
  2. ^ 1930 Canadian patent CA 304755 by Hubert Townend with drawings
  3. ^ "A History of Aircraft Piston Engines" by Herschel Smith, (Sunflower University Press Manhattan, Kansas, 1981, ISBN 0-89745-079-5), 255pp.
  4. ^ Hansen, James R. "Engineering Science and the Development of the NACA Low-Drag Engine Cowling". From Engineering Science to Big Science: The NACA and NASA Collier Trophy Research Project Winners. Archived from the original on 2004-10-31. Retrieved 2007-04-28. 

External links

  • The Spotters Glossary
  • North, J D (8 February 1934), "Engine Cowling: With Special Reference to the Air-cooled Engine", The Aircraft Engineer (Supplement to Flight), XXIV No. 6 (1311): 133–137 
  • North, J D (22 February 1934), "Engine Cowling", The Aircraft Engineer (Supplement to Flight), IX No. 2 (97): 174a–174f 
  • "Engine Cowling", Flight, XXVI No. 7 (1312), 15 February 1934: 157–158 

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