NASA/CR-4671, Lucas, M.J. and Noreen, R. and Southerland, L.D. and Cole III, J. and Junger, M., The Acoustic Characteristics of Turbomachinery Cavities, Prepared for Structures and Dynamics Laboratory, Science and Engineering Directorate, NASA Marshall Space Flight Center, AL 35812, Contract NAS8-37360, by Wyle Research 2001 Jefferson Davis Highway, Suite 701 Arlington, VA 22202, May, 1995, pp. 317, Format(s): PDF 8902k |
Internal fluid flows are subject not only to self-sustained oscillations of the purely hydrodynamic type but also to the coupling of the instability with the acoustic mode of the
surrounding cavity. This situation is common to turbomachinery, since flow instabilities are confined within a flow path where the acoustic wavelength is typically smaller than the dimensions of the cavity and flow speeds are low enough to allow resonances. When acoustic coupling occurs, the fluctuations can become so severe in amplitude that it may induce structural failure of engine components. The potential for catastrophic failure makes identifying flow-induced noise and vibration sources a priority. In view of the complexity of these types of flows, this report was written with the purpose of presenting many of the methods used to compute frequencies for self-sustained oscillations. The report also presents the engineering formulae needed to calculate the acoustic resonant modes for ducts and cavities. Although the report is not a replacement for more complex numerical or experimental modeling techniques, it is intended to be used on general types of flow configurations that are known to produce self-sustained oscillations. This report provides a complete collection of these models under one cover.
| Keywords: | vortex shedding, edgetone, unsteady flow, acoustics, oscillation, flow instability, turbomachine, turbopump |
|---|---|
| CASI Document ID Number: | 95N28720 |
| Subjects: | Aeronautics: Aerodynamics |
| ID Code: | 281 |
| Deposited On: | 27 June 2002 |