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.
IN the design of long range aircraft, the high percentage weight of fuel carried lias always tended to necessitate the provision of a system by means of which this fuel could be rapidly jettisoned, in the event of forced landing or continued flight on partial power. The provision of such a jettison system is now an important problem in ancillary design.
Aircraft Engineering and Aerospace Technology – Emerald Publishing
Published: Sep 1, 1941
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.