Advances in THRUST AUGMENTATION for RADIAL ENGINE INSTALLATIONS

480174

01/01/1948

Event
Pre-1964 SAE Technical Papers
Authors Abstract
Content
THE exhaust thrust augmentor developed for the Convair 240 airplane overcomes cooling drag and adds enough thrust to increase level flight 10 mph and take-off payload 2000 lb. It provides sufficient hot air for complete cabin heat, and wing and tail anti-icing.
In the Convair design, there are two ejectors, each one receiving exhaust from three triamese stacks.
Cantilever cowling developed in conjunction with the ejector provides excellent sealing plus complete access to cylinders, spark plugs, and exhaust stacks.
Meta TagsDetails
DOI
https://doi.org/10.4271/480174
Pages
12
Citation
CLEGERN, W., "Advances in THRUST AUGMENTATION for RADIAL ENGINE INSTALLATIONS," SAE Technical Paper 480174, 1948, https://doi.org/10.4271/480174.
Additional Details
Publisher
Published
Jan 1, 1948
Product Code
480174
Content Type
Technical Paper
Language
English