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The whistler nozzle phenomenonThe whistler nozzle is a simple device which can induce jet self-excitations of controllable amplitudes and frequencies and appears highly promising for many applications involving turbulent transport, combustion and aerodynamic noise. The characteristics of this curious phenomenon are documented for different values of the controlling parameters and attempts to explain the phenomenon. It is shown that the whistler excitation results from the coupling of two independent resonance mechanisms: shear-layer tone resulting from the impingement of the pipe-exit shear layer on the collar lip, and organ-pipe resonance of the pipe-nozzle. The crucial role of the shear-layer tone in driving the organ-pipe resonance is proven by reproducing the event in pipe-ring and pipe-hole configurations in the absence of the collar. It is also shown that this phenomenon is the strongest when the self-excitation frequency matches the preferred mode of the jet.
Document ID
19830012435
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hussain, A. K. M. F.
(Houston Univ. TX, United States)
Hasan, M. A. Z.
(Houston Univ. TX, United States)
Date Acquired
September 4, 2013
Publication Date
October 1, 1982
Subject Category
Acoustics
Report/Patent Number
FM-15
NAS 1.26:170015
NASA-CR-170015
Report Number: FM-15
Report Number: NAS 1.26:170015
Report Number: NASA-CR-170015
Accession Number
83N20706
Funding Number(s)
CONTRACT_GRANT: NAG3-198
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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