https://ntrs.nasa.gov/search.jsp?R=19790023885 2018-11-28T00:54:20+00:00Z NASA Effect Acoustic Impedance of Helmholtz Resonators Consisting of Single and Clustered Orifices Alan S. Hersh and Bruce Walker CONTRACT NAS3-19745 AUGUST 1979 _.I. ‘, I ‘>J , ‘.. _” :“. , ‘. ‘.. I, IUASA ._ : _. : . . ..: TECH LIBRARY KAFB, NM NASA Contractor Report 3177 Effect of Grazing Flow on the Acoustic Impedance of Helmholtz Resonators Consisting of Single and Clustered Orifices Alan S. Hersh and Bruce Walker Herd Acoustical Engineering Cha tsworth, Culiforizia Prepared for Lewis Research Center under Contract NAS3-19745 National Aeronautics and Space Administration Scientific and Technical information Branch 1979 TABLE OF CONTENTS SUMMARY.. .................................................. 1 DEFINITION OF SYMBOLS. ..................................... 2 1. INTRODUCTION ............................................... 5 2. SINGLE ORIFICE IMPEDANCE MODEL. ............................ 7 2.1 Derivation of Governing Equations .................... 8 2.2 Boundary Conditions .................................. 12 2.3 Semi-empirical Solution .............................. 13 3. SINGLE ORIFICE MEASUREMENT PROGRAM.. ....................... 17 3.1 Two-Microphone Method ................................ 18 3.2 Determination of CD .................................. 20 3.3 Comparison Between Predicted and Measured Impedance . . 25 3.4 Thick Orifices ....................................... 29 3 .. 5 Resonator Self-Noise ................................. 31 4. IMPEDANCE OF CLUSTERED ORIFICES ............................ 32 4.1 Zero Grazing Flow, Low Sound Amplitude Results ....... 33 4.2 Effect of Grazing Flow ............................... 35 5. CONCLUSIONS ................................................ 38 APPENDIXES A- SINGLE ORIFICE DATA .................................. 40 B- SUMMARY OF FREQUENCY SWEEP DATA FOR SPECIAL MODEL FOR V," = 60 m/set and P$ = 120 dB .................. 66 c - THICK ORIFICE DATA.........,. ......................... 67 D- CLUSTERED ORIFICE DATA ............................... 76 REFERENCES. ................................................ 104 TABLES ..................................................... 106 FIGURES.................................................... 110 iii I -- SUMMARY A semi-empirical fluid mechanical model is derived for the acoustic behavior of thin-walled single orifice Helmholtz reson- ators in a grazing flow environment. The model assumes that the flow field incident to a resonator orifice consists of a spheri- cal sound particle velocity field superimposed upon a mean graz- ing flow. The incident and cavity sound fields are connected in terms of an orifice discharge coefficient whose values are deter- mined experimentally using the two-microphone method. With re- gard to its application to aircraft engines, the most important finding of this study is that at high grazing flow speeds, acous- tic resistance is almost linearly proportional to the grazing flow speed and almost independent of incident sound pressure. The corresponding values of reactance are much smaller and tend towards zero for increasing grazing flow speed. Because of their insen- sitivity to the incident sound, the impedance of Helmholtz resona- tors at high grazing flow speeds is almost "linear". The effects of grazing flow on the acoustic behavior of thick-walled single orifice Helmholtz resonators were studied ex- perimentally. Test results showed both resistance and reactance to become increasingly less sensitive to the grazing flow as the ratio of plate thickness to orifice diameter increased. Loud resonant tones were observed to radiate from single orifice Helmholtz resonators due to interaction between the graz- ing flow shear layer and the resonator cavity. The tones occurred at a grazing flow speed defined as (Vz)res=f*e d*/0.26 where f;,, is the resonator classical Helmholtz resonan F zrequency and d* is the orifice diameter. Measurements show that for grazing flow speeds greater than (Vz)res, the grazing flow dominates the resona- tor behavior and for grazing flow speeds less than (Vz)r the sound particle velocity field dominates the resonator be@cior. The two-microphone method was also used to measure the effect of grazing flow on the impedance of Helmholtz resonators consisting of clusters of orifices. The study showed that inter- action between nearby orifices occur only for those orifices whose centers are aligned parallel to the grazing flow. Interaction does not occur for orifices whose centers are aligned perpendi- cular to the grazing flow. In general, both resistance and reactance are virtually independent of orifice relative spacing and number. Orifice end correction, on the other hand, is quite dependent upon orifice spacing. It is fairly insensitive to the number of orifices. These findings are valid with and without grazing flow. 1 DEFINITION OF SYMBOLS Symbol Definition orifice area; also Fok area defined by Fig. 1. A; Af A min minimum area enclosed by orifices C speed of sound (meters/set) discharge coefficient defined by Eq. (8) =D d diameter of coefficient (meters) de orifice inertial length (meters) D diameter of cylindrical cavity (meters) E small parameter defined by Eq. (8) ? small parameter defined by Eq. (26) bl special parameter defined by Eq. (28b) f(t); f special function defined by Eq. (14); also frequency F(t) function of time defined by Eq. (29) G (t> special function defined by Eq. (24) L cavity depth (meters) resonator characteristic length (meters) Le grazing flow Mach number (VJc) Men N number of orifices backed by a common cavity P acoustic pressure (Newtons/meters') pi amplitude of incident sound wave (Newtons/ meters') amplitude of cavity sound wave (Newtons/ PC meters*) sound particle velocity 9’ (meters/set) r radial coordinate (meters) orifice area-averaged acoustic resistance RO (Kg/meters*/sec) s; Sf separation distance between adjacent array (m); Fokseparation parameter defined in Fig. 1. orifice area (meters') SO S orifice vena contracta area (meters*) vc defined in Fig. 8 (meters) SC0 t time (set) 2 Symbol Definition U acoustic particle velocity at orifice vc vena contracta (meters/set) radial, polar, azimuthal acoustic particle u,v,w velocity components (meters/set) resonator cavity volume (meters3) % grazing flow speed (meters/set) Ym resonator orifice inertial length (meters) de resonator orifice area-averaged reactance xO (Kg/meters2/sec) resonator orifice area-averaged impedance (Kg/meters2/sec) parameter defined by Eq. (20) small parameter defined by Eq. (8) fluid density (Kg/meters3) grazing flow boundary-layer thickness (meters) orifice end correction (meters) orifice array interaction parameter (d/D) incident sound field radian frequency (Hz) nondimensional parameter defined by Eq. (46) resonator orifice percent open area orifice plate thickness (meters) Fok interaction function spherical coordinate polar angle spherical coordinate azimuthal angle phase angle shift across orifice (deg.) Subscripts i incident C cavity N refers to N orifices BL boundary layer 0 orifice o,N orifice referenced to N res refers to resonator resonant frequency V.C. refers to orifice vena contracta 3 Subscripts Definition t refers to total resonator Superscripts ( I' refers to fluctuating quantities ( I* refers to dimensional quantities 4 1. INTRODUCTION The application of arrays of cavity-backed orifices as sound absorbing devices in the inlet and exhaust of jet engines has gen- erated the need to understand their acoustic behavior in a high speed grazing flow environment. This need has prompted a number of research investigations aimed at predicting the effect of graz- ing flow on the impedance of isolated orifices. Early experimen- tal studies by Mechel, Mertens and Schilz', Phillips2, Ronneberger3 and Dean4 showed that relative to their zero grazing flow values, the effects of grazing flow are to increase orifice resistance and decrease orifice reactance. Dean noted that some of the reson- ators exhibited an increase in reactance with grazing flow while others exhibited a decrease. He offered no explanation for this. Recent studies by Rogers and Hersh5, Baumeister and Rice6, Hersh and Rogers' and Rice have added greatly to our understanding of the acoustic behavior of Helmholtz resonators in a grazing flow environment. Rogers and Hersh correlated measurements of the steady- state resistance of isolated square-edged orifices in a grazing flow environment in terms of an effective orifice discharge coefficient. By introducing a simple inviscid model based on this airfoil theory to account for the interaction between the grazing flow and the orifice inflow and outflow, Rogers and Hersh showed that the dis- charge coefficient decreased to very small values relative to its classical zero grazing flow speed value of near 0.6. Rogers and Hersh showed by means of simple flow visualization techniques that the reduction in CD results from a blockage of the orifice area by interaction between the grazing flow and the orifice inflow and outflow in the form of complicated eddies. Baumeister and Rice conducted a very detailed visual study of interaction between a steady-state grazing flow and an oscilla- ting orifice flow. Flow visualization was achieved by constructing a flow channel and a single orifice side branch Helmholtz resonator out of plexiglass and using water as the fluid medium. An oscilla- tory flow was applied to the resonator cavity and color dyes were injected in both the orifice and the grazing flow. High speed cameras were used to record the motion of the fluid. An impor- tant finding of their study is that interaction between the steady- state grazing flow and the oscillating orifice inflow and outflows reduced the orifice effective open area. Hersh and Rogers derived a fluid mechanical model of the acoustic behavior of isolated circular orifices for the.case of 5 II non-grazSng flow. By assuming that the sound particle velocity field approaches the orifice.as a spherically symmetric radial flow, they showed to lowest order that the particle velocity field near the orifice is incompressible and unsteady. They further showed that at high incident sound pressure levels, the particle velocity is nonlinear. In this regime, the resistance, proportion- al to the square root of the amplitude of the incident sound pres- sure field, is much larger than the orifice inertial reactance or the cavity stiffness reactance. Rice extended the work of Hersh and Rogers to include the effects of a high speed grazing flow. He derived a physically meaningful solution by assuming that the velocity field consists of a spherically symmetric particle velocity component superim- posed upon a uniform grazing flow. Rice showed that when the grazing flow speed is sufficiently large (relative to the ampli- tude of the sound particle velocity field), the orifice resistance is linearly proportional to the grazing flow speed and independent of the amplitude of the incident sound. The above review dealt only with isolated orifices. Pre- vious work related to the effects of multiple or clustered ori- fices is discussed below. In the application of cavity-backed orifices as sound absorbing devices, possible interaction among neighboring orifices has been traditionally ignored in the design process, probably because of the lack of available data to assess its importance. This is especially true for the intense sound pressure levels and high grazing flows within jet engines. A review of the literature indicates that the p;evious studies of interacting orifices, conducted by Ingard and Fok" considered only the special cases of zero grazing flow (V* =0) and low sound pressure levels (i.e., the linear regime). oDMellinll recently reviewed their models. Briefly, both Ingard and Fok derived theoretical expressions for the interaction. Ingard's solutions indicate that the orifice end correction is strongly dependent upon the spacing between orifices. Mellin applied Fok's model to derive the following expression for the Helmholtz- type specific reactance x*, (igncring the small viscous contribu- tion), (11 where p* is the fluid density, U* the radian sound frequency, u is the plate porosity, r* is the plate thickness, d* the (circu- lar) orifice diameter, de* is the orifice effective inertial length, and I+'(C) is the Fok interaction function defined in Fig. 1. Herei=d*/S*f is an interaction parameter where d* is 6