Hostname: page-component-7479d7b7d-fwgfc Total loading time: 0 Render date: 2024-07-11T02:27:34.938Z Has data issue: false hasContentIssue false
  • English
  • Français

Leakage Rates from a Pressurised Aircraft at Altitude

Published online by Cambridge University Press:  28 July 2016

L. R. Jenkins
L. R. Jenkins*
Affiliation:
Aeroplane and Armament Experimental Establishment, Boscombe Down
Get access Rights & Permissions [Opens in a new window]

Extract

Flight tests were made to verify a method of predicting pressure cabin leakage rates at altitude from ground test results proposed in a Technical Note published in The Journal in August 1954 The results showed very good agreement with the theoretical treatment of the problem.

It is therefore recommended that the method of the Technical Note be used to estimate the change of leakage rates with altitude and also to estimate the time for the excess pressure to fall during a descent with no pressure supply.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 61 , Issue 563 , November 1957 , pp. 776 - 779
Copyright
Copyright © Royal Aeronautical Society 1957

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1. Staite, H. J. (1954). Leakage Rates from Pressurised Aircraft at Altitude. Technical Note, Journal of the Royal Aeronautical Society, August 1954.CrossRefGoogle Scholar
2. Hughes, D. P. (1956). Leakage Rates from Pressurised Aircraft at Altitude–Comment Correction by Staite, H. J.. Journal of the Royal Aeronautical Society, June 1956.Google Scholar