Hostname: page-component-848d4c4894-nmvwc Total loading time: 0 Render date: 2024-07-06T05:22:52.252Z Has data issue: false hasContentIssue false
  • English
  • Français

The Three-Shock Confluence on a Simple Wedge Intake

Published online by Cambridge University Press:  07 June 2016

L. F. Henderson
L. F. Henderson*
Affiliation:
Department of Mechanical Engineering, University of Sydney
Get access

Summary

Results obtained from previous studies of the three-shock confluence are applied to a simple wedge intake with the objective of obtaining a qualitative description of the flow for given initial conditions (M0, δ0). A simple mapping procedure is used, so that when M0, δ0 varies slowly and continuously the resulting effect on the shock geometry can be discussed in a systematic fashion. A number of special curves are computed to help classify various regions of initial conditions.

Type
Research Article
Information
Aeronautical Quarterly , Volume 16 , Issue 1 , February 1965 , pp. 42 - 54
Copyright
Copyright © Royal Aeronautical Society. 1965

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. Oswatitsch, K. Der Druckwiedergewinn bei Geschossen mit Ruckstossantrieb bei hohen Uberschallgeschwindigkeiten (Der Wirkungsgrad von Stossdiffusoren). Deutsche Versuchsanstalt für Luftfahrt, Bericht 49, 1957 (first published in 1944).Google Scholar
2. Henderson, L. F. On the Confluence of Three Shock Waves in a Perfect Gas. Aeronautical Quarterly, Vol. XV p. 181, May 1964.CrossRefGoogle Scholar
3. Weise, A. Theorie des gegabelten Verdichtungstosses. Jahrbuch de Deutsche Luftfahrt-Forschung 1943. Also in Zentralstelle Wissenschaftliche Berichte (Z.W.B.), Vol. 10, Part 12, Appendix lla, 1943.Google Scholar
4. Eggink, H. Uber Verdichtungstosse bei abgeloster Strömung. Zentralstelle Wissenschaftliche Berichte (Z.W.B.) 1850, Aachen, 1943.Google Scholar
5. Wuest, W. Zur Theorie des gegabelten Verdichtungstosses. Zeitschrift fiir Angewandte Mathematik und Mechanik, Vol. 28, No. 3 p. 73, 1948.Google Scholar
6. Wecken, F. Grenzlagen gegabelter Verdichtungstosses. Zeitschrift fiir Angewandte Mathematik und Mechanik, Vol. 29, No. 5 p. 147, 1949.Google Scholar
7. Courant, R. Differential and Integral Calculus, Vol. II. Blackie, 1950.Google Scholar
8. Guderley, K. G. Consideration on the Structure of Mixed Subsonic-Supersonic Flow Patterns. Technical Report F-TR-2168-ND, Headquarters Air Materiel Command, Wright Field, Dayton, Ohio, U.S.A., 1947.Google Scholar
9. Pain, H. J. and Rogers, E. W. E. Shock Waves in Gases. Reports on Progress in Physics (The Institute of Physics and the Physical Society), Vol. XXV p. 287, 1962.Google Scholar
10. Guderley, K. G. The Theory of Transonic Flow. Pergamon Press, 1962.Google Scholar
11. Courant, R. and Friedrichs, K. O. Supersonic Flow and Shock Waves. Interscience Publishers, New York, 1948.Google Scholar