The Reduction of Position Error: An Examination of the Points to be Watched when Installing a Pitot‐Static Head

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Publication date: 1 August 1939

Abstract

RECENT tendencies in the design and operating conditions of aircraft have laid increasing emphasis on the short‐comings of the generally accepted pitot‐static method of measuring flight speed. The routine use of air navigation over long distances has spread widely during the past ten years, and, as a result of the greater distances involved, the percentage error in measured flight speed which can be tolerated has become smaller. This un‐satisfactory position was not until quite recently relieved by any very clear appreciation of the errors involved in fitting a pitot‐static head in any given position on an aircraft.

Citation

Kenney, K. (1939), "The Reduction of Position Error: An Examination of the Points to be Watched when Installing a Pitot‐Static Head", Aircraft Engineering and Aerospace Technology, Vol. 11 No. 8, pp. 309-313. https://doi.org/10.1108/eb030526

Publisher

:

MCB UP Ltd

Copyright © 1939, MCB UP Limited

To read the full version of this content please select one of the options below

You may be able to access this content by logging in via Shibboleth, Open Athens or with your Emerald account.
To rent this content from Deepdyve, please click the button.
If you think you should have access to this content, click the button to contact our support team.