Published 1974 | Version Accepted Version
Technical Report Open

The generation of noise by the fluctuations in gas temperature into a turbine

Abstract

An actuator disc analysis is used to calculate the pressure fluctuations produced by the convection of temperature fluctuations (entropy waves) into one or more rows of blades. The perturbations in pressure and temperature must be small, but the mean flow deflection and acceleration are generally large. The calculations indicate that the small temperature fluctuations produced by combustion chambers are sufficient to produce large amounts of acoustic power. Although designed primarily to calculate the effect of entropy waves, the method is more general and is able to predict the pressure and vorticity waves generated by upstream or downstream going pressure waves or by vorticity waves impinging on blade rows.

Additional Information

© 1974, The authors wish to thank Dr. D.S. Whitehead for his help in discussing some aspects of this work, and in particular for his assistance with the method of solution. The help of Drs. R.R. Dils and E.M. Greitzer of Pratt and Whitney aircraft is greatly appreciated.

Attached Files

Accepted Version - 259_Cumpsty_NA_1974.pdf

Files

259_Cumpsty_NA_1974.pdf

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Additional details

Identifiers

Eprint ID
21895
Resolver ID
CaltechAUTHORS:20110126-092110939

Dates

Created
2011-02-09
Created from EPrint's datestamp field
Updated
2019-10-03
Created from EPrint's last_modified field

Caltech Custom Metadata

Caltech groups
Guggenheim Jet Propulsion Center
Series Name
Report CUED/A TURBO/TR
Series Volume or Issue Number
57
Other Numbering System Name
Guggenheim Jet Propulsion Center