Hostname: page-component-586b7cd67f-2brh9 Total loading time: 0 Render date: 2024-12-01T03:27:08.644Z Has data issue: false hasContentIssue false
  • English
  • Français

The possibility of the determination of rate of climb from acceleration measurements in level flight

Published online by Cambridge University Press:  07 June 2016

E. C. Pike
E. C. Pike*
Affiliation:
Member of the Technical Staff of the Royal Aeronautical Society
Get access

Summary

Performance measurements for turbo-jet and turbo-prop aircraft are most conveniently reduced to standard conditions by the use of graphical methods. The case of rate of climb presents difficulties if readings are taken in the normal way during continuous climbs, because of the variation of weight, temperature, pressure and optimum climbing speed with height.

Since rate of climb is proportional to the product of speed and acceleration in level flight, these quantities could be measured and used to determine the rate of climb at any height.

The advantages of the method are listed and the technique required of the pilot examined. An automatic observer, including a longitudinal accelerometer, reading, in some cases, to within 0.001g, is necessary.

Type
Research Article
Information
Aeronautical Quarterly , Volume 2 , Issue 1 , May 1950 , pp. 15 - 22
Copyright
Copyright © Royal Aeronautical Society. 1950

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. Royal Aeronautical Society’s Performance Data Sheets.Google Scholar
2. Smith, F. (1943). Note on various Methods of Performance Reduction for Jet-Propelled Aircraft (with addendum). R.A.E. Tech. Note. No. Aero. 1348 and 1348a, 1943.Google Scholar
3. Pike, E. C. (1949). Note on Propeller Turbine Reduction Methods. The Aeronautical Quarterly, Vol. I, May 1949.Google Scholar