Hostname: page-component-848d4c4894-wzw2p Total loading time: 0 Render date: 2024-05-06T03:23:54.840Z Has data issue: false hasContentIssue false
  • English
  • Français

Instrumentation for Testing Aircraft and Aero-Engines*

Published online by Cambridge University Press:  28 July 2016

C. N. Jaques
C. N. Jaques*
Affiliation:
Instrument and Photographic Department, Royal Aircraft Establishment
Get access Rights & Permissions [Opens in a new window]

Extract

The term Aircraft Instrumentation is used to describe the special instruments which in a variety of circumstances are needed to determine aerodynamic, structural and power plant characteristics. Such circumstances may be flight tests of prototype aircraft, tests in the air or on the ground of the aeroplane, its structure or power plant, or the acquisition of statistical data on the conditions to which aircraft are subjected in civil or military operation. These special instruments therefore are additional to, and usually different from, the instruments needed in an aeroplane to enable it to fulfil its military or civil role.

Type
Research Article
Information
The Aeronautical Journal , Volume 55 , Issue 492 , December 1951 , pp. 762 - 781
Copyright
Copyright © Royal Aeronautical Society 1951

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.)

Footnotes

*

A Joint Lecture to the Southampton Branch of the Royal Aeronautical Society and to the Southern Branches of the Institution of Electrical Engineers and the Institution of Mechanical Engineers on 11th April 1951.

References

* A Joint Lecture to the Southampton Branch of the Royal Aeronautical Society and to the Southern Branches of the Institution of Electrical Engineers and the Institution of Mechanical Engineers on 11th April 1951.