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A Theory of the Cylindrical Ejector Supersonic Propelling Nozzle

Published online by Cambridge University Press:  04 July 2016

H. Pearson ,
J. B. Holliday  and
S. F. Smith
H. Pearson
Affiliation:
Aero Engine Division, Rolls-Royce Ltd.
J. B. Holliday
Affiliation:
Aero Engine Division, Rolls-Royce Ltd.
S. F. Smith
Affiliation:
Aero Engine Division, Rolls-Royce Ltd.
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Extract

The so-called ejector nozzle has received a large amount of experimental study as a means for achieving efficient supersonic expansion of the main jet without the difficulties of a mechanically variable convergentdivergent nozzle. No satisfactory theory for the calculation of its performance has yet been put forward and it is the object of this paper partly to remedy this defect.

Type
Research Article
Information
The Aeronautical Journal , Volume 62 , Issue 574 , October 1958 , pp. 746 - 751
Copyright
Copyright © Royal Aeronautical Society 1958

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