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An Energy Approach to Climb Performance Estimation of a Turbo-Jet Transport Aircraft

Published online by Cambridge University Press:  07 June 2016

Ramchandra B. Tamboli
Ramchandra B. Tamboli*
Affiliation:
de Havilland Aircraft, Hatfield
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Summary

The climb performance of a turbo-jet transport aircraft is considered, using the concept of the energy height. The analytical formulae used in evaluating the time needed, distance covered and fuel consumed during climb under various conditions are developed. It is concluded that the application of this energy approach method to the climb performance estimation of a turbojet transport aircraft will prove satisfactory from the points of view both of the accuracy of the results and of saving some of the considerable time needed for the climb calculation by the conventional method. A numerical example is given to illustrate the usefulness, applicability and flexibility of this method.

Type
Research Article
Information
Aeronautical Quarterly , Volume 7 , Issue 4 , November 1956 , pp. 315 - 336
Copyright
Copyright © Royal Aeronautical Society. 1956

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References

1. Rutowski, E. S. Energy Approach to General Aircraft Performance Problems. Journal of the Aeronautical Sciences, Vol, 21, No. 3, pp. 187–195, March 1954.CrossRefGoogle Scholar
2. Kelly, L. Optimum Climb Technique for a Jet Propelled Aircraft. The College of Aeronautics, Cranfield, Report No. 57, April 1952.Google Scholar
3. Lush, K. J. A Review of the Problem of Choosing a Climb Technique With Proposals for a New Climb Technique for High Performance Aircraft. R. & M. 2557, 1951.Google Scholar