Access the full text.
Sign up today, get DeepDyve free for 14 days.
References for this paper are not available at this time. We will be adding them shortly, thank you for your patience.
The radiator b of a liquidcooled aircraft engine is housed in a tunnellike cowling bl, through which the slip stream flows by a contracted entrance and exit b3, b6 and into which the exhaust is discharged by nozzles the exhaust system thus has less drag on the aircraft, and the air flow past the radiator is increased. The radiator is of horseshoe shape in crosssection, and inclined and Venturishaped slats b4, 1 are provided to steady the air flow and to act as silencers and flame dampers, The exhaust may be led by Dsectioned pipes d1 arranged within the contour of the cowling, but separated therefrom by a coolingair space. Alternatively the pipes may be circular and located inside the cowling they are surrounded by jackets through which air is led by diverging intakes in the air stream and from which it is discharged behind the radiator. An oil cooler g is arranged in the cowling underneath the radiator. The two exhaust pipes of a Vengine extend down the two sides of the cowling and are united to the pipe having the nozzles .
Aircraft Engineering and Aerospace Technology – Emerald Publishing
Published: Dec 1, 1936
Read and print from thousands of top scholarly journals.
Already have an account? Log in
Bookmark this article. You can see your Bookmarks on your DeepDyve Library.
To save an article, log in first, or sign up for a DeepDyve account if you don’t already have one.
Copy and paste the desired citation format or use the link below to download a file formatted for EndNote
Access the full text.
Sign up today, get DeepDyve free for 14 days.
All DeepDyve websites use cookies to improve your online experience. They were placed on your computer when you launched this website. You can change your cookie settings through your browser.