Hostname: page-component-586b7cd67f-t7fkt Total loading time: 0 Render date: 2024-11-25T01:43:24.260Z Has data issue: false hasContentIssue false
  • English
  • Français

Perturbations of Supersonic Nozzle Flows

Published online by Cambridge University Press:  07 June 2016

R. E. Meyer
R. E. Meyer*
Affiliation:
Department of Aeronautics, University of Sydney
Get access

Summary

Small, steady perturbations of general two-dimensional steady, shock-free, supersonic flows are studied and the perturbation fields of symmetrical nozzle flows are described in detail. The relation between errors in the shape of the supersonic part of the nozzle liners and the deviations from uniformity of the flow in the test section is given to an approximation sufficient for the treatment of a number of problems arising from experiment and in the design of nozzles.

Type
Research Article
Information
Aeronautical Quarterly , Volume 7 , Issue 1 , February 1956 , pp. 71 - 84
Copyright
Copyright © Royal Aeronautical Society. 1956

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. Meyer, R. E. and Holt, M. The Correction of Wind-Tunnel Nozzles for Two-Dimensional Supersonic Flow. The Aeronautical Quarterly, Vol. II, pp. 195–208, November 1950.Google Scholar
2. Howarth, L. (Editor). Modern Developments in Fluid Dynamics, High Speed Flow, Vol. I, Chap. III. Oxford University Press, 1953.Google Scholar
3. Meyer, R. E. Focusing Effects in Two-Dimensional, Supersonic Flow. Phil. Trans., 242A, pp. 153–171, 1949.Google Scholar
4. Hall, M. G. The Accuracy of the Numerical Method of Characteristics for Two- Dimensional, Supersonic Flow. Aeronautical Research Laboratories, Melbourne, Report A.95, 1955.Google Scholar
5. Meyer, R. E. and Mahony, J. J. Analytical Treatment of Two-Dimensional, Supersonic Flow. Phil. Trans. In the press, 1955.Google Scholar
6. Lighthill, M. J. The Hodograph Transformation in Transonic Flow. Part I, Symmetrical Channels. Proc. Roy. Soc, A, Vol. 191, pp. 323–341, 1947.Google Scholar
7. Cherry, T. M. A Transformation of the Hodograph Equation and the Determination of Certain Fluid Motions. Phil. Trans., 245A, pp. 583–626, 1953.Google Scholar
8. Meyer, R. E. Turbulent Boundary Layer Growth on Nozzle Liners. Journal of the Aeronautical Sciences, Vol. 22. In the press, 1955.Google Scholar