The Three-Shock Confluence on a Simple Wedge Intake
- 1 February 1965
- journal article
- research article
- Published by Cambridge University Press (CUP) in Aeronautical Quarterly
- Vol. 16 (1), 42-54
- https://doi.org/10.1017/s0001925900003279
Abstract
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.Keywords
This publication has 4 references indexed in Scilit:
- On the Confluence of Three Shock Waves in a Perfect GasAeronautical Quarterly, 1964
- Shock waves in gasesReports on Progress in Physics, 1962
- Grenzlagen gegabelter VerdichtungsstößeZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik, 1949
- Zur Theorie des gegabelten VerdichtungsstoßesZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik, 1948