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Nonstationary gas flow with shock waves in a supersonic compressor
- Source :
- Journal of Applied Mechanics and Technical Physics; September 1973, Vol. 14 Issue: 5 p636-641, 6p
- Publication Year :
- 1973
-
Abstract
- Shock waves are formed in the channels between blades in a compressor working in the transsonic state, and the positions of these vary periodically and produce strong vibrations in the blades. The effect is extremely complex and is dependent on a large number of parameters. Here we present a simplified model for the effect, which can be examined theoretically. It is assumed that the nonstationary pulsations in the flow and the amplitudes in the oscillations of the shock waves are small, and therefore one can employ a steady-state flow whose characteristics may be taken as given, including the mean position of the shock waves.
Details
- Language :
- English
- ISSN :
- 00218944 and 15738620
- Volume :
- 14
- Issue :
- 5
- Database :
- Supplemental Index
- Journal :
- Journal of Applied Mechanics and Technical Physics
- Publication Type :
- Periodical
- Accession number :
- ejs16895464
- Full Text :
- https://doi.org/10.1007/BF00856873