INDEX TO VOLUME
16
AHMED,K. M., On the energy functions for curved sandwich plates (letter) . . . (3)461 ANDERSON,G. L. On the forced vibrations of elastic bodies in contact . . . . (4) 533 ANNOUNCEMENTS. . . . . . . . . . . . (1) 137, (4)645 ATTENBOROUGH,K., The influence of microstructure on propagation in porous fibrous absorbents . . . . . . . . . . . . . (3)419 BAADE,P. K., Equipment sound power measurements in reverberation rooms . . (I) 131 BATES,R. H. T., A theorem for wide bandwidth echo-location systems . . . . (2) 223 BAZLEY,E. N., See DELANY,M. E. . . . . . . . . . . (3)315 (2) 293 CRAGGS, A., The response of a simply supported plate to “N” waves at oblique incidence CREMER,L., The second annual Fairey lecture: the treatment of fans as black boxes . (1) 1 DASARATHY,B. V., Equivalent higher order linear and non-linear systems . . . (4) 623 DELANY, M. E. AND BAZLEY,E. N., A note on the effect of ground absorption in the measurement of aircraft noise . . . . . . . . . (3)315 DENISE,J.-P., See P~;~DOUSSIS, M. P. . . . . . . . . . . (3)459 DICKINSON,S. M., Lateral vibration of rectangular plates subject to in-plane forces. . (4) 465 DoAK,P.E.,%xDoDD,S.D.. . . . . . . . . . . (1) 89 DODD, S. D. ANDDOAK, P. E., Some aspects of the theory of diffusion and diffusers . (I) 89 EBBING,C. E., Experimental evaluation of moving sound diffusers for reverberant rooms. (1) 99 EFSTATHIADES,G. J., A new approach to the large-deflection vibrations of imperfect circular disks using Galerkin’s procedure. . . . . . . . (2)231 (3)407 FISHER, M. J., See MATHER,J. S. B. . HENSHALL,R. D., NEALE, B. K. AND WARBURTON,G: B., i new’hybrfd cylihdrical sheli finite element . . . . (4)519 . . . . . . . Hsu, T.-M. ANDWANG, J. T.-S., Rotationally symmetric vibrations of orthotropic layered cylindrical shells . . (4) 473 . . . . . . . . . KADI, A. S., See LEISSA,A. W.’ . . . . . . . . . . (2) 173 KILDAL, A., On the three-dimensional streaming motion set up by a vibrating plate. . (2) 149 KOOPMAN,G. AND POLLARD,H., Model studies of Helmholtz resonators in rooms with windows and doorways. . . . . . . . . . , (4) 489 LEISSA,A. W. AND KADI, A. S., Curvature effects on shallow shell vibrations . . (2) 173 LINDEN,T. L. J., See MAESTRELLO, L. . . . . . . . & 165, 385 LONG, B. R., A stiffness-type analysis of the vibration of a class of stiffened plates . . (3) 323 LUBMAN,D., Spatial averaging in sound power measurements . . . . . (1) 43 MAESTRELLO, L. ANDLINDEN,T. L. J., Measurements of the response of a panel excited by shock boundary-layer interaction _ . . . . . . . . (3) 385 MAESTRELLO, L. ANDLINDEN,T. L. J., Response of an acoustically loaded panel excited by supersonically convected turbulence . . . . . . . . (3) 365 MALING, G. C., JR, Computer studies of mode-spacing statistics in reverberation rooms . (1) 79 MATHER,J. S. B., SAVID~E,J. ANDFISHER, M. J., New observations on tone generation in fans . . . . . . . . . . . . . (3)407 MOORE,C. J., A solution to the problem of measuring the sound field of a source in the presence of a ground surface . . . . . . . . . _ (2) 269 MoRFEY,C.L.,S~~TANNA,H.K. . . . . . . . . . . (3) 337 MORROW,C. T., Point-to-point correlation of sound pressures in reverberation chambers (1) 29 MUGRIDGE,B. D., Acoustic radiation from aerofoils with turbulent boundary layers . (4) 593 MULLER,J. L., Calculation of aircraft noise duration . . . _ . . . (4) 581 NEALE,B. K., See HENSHALL,R. D. . . . . . . _ . . . (4)519 NEWALL,A. F., See WESTON,R. H. . . . . . . . . . (3) 443 PAIDOUSSIS,M. P. AND DENISE,J.-P., Flutter of &lindrical shells conveying fluid (letter) . (3) 459 POLLARD,H., See KOOPMAN,G. . . . . . . . . _ . (4) 489 RAINER,J. H., Dynamic ground compliance in multistorey buildings . . . . (4)615 RAO, S. S., Effects of transverse shear and rotatory inertia on the coupled twist-bending vibrations of circular rings . . . . . . . . . . (4) 551 SARGENT,J. W., See SCHOLES,W. E. . . . . . _ _ . . (4) 627 651
652
INDEX TO VOLUME16
SALVIDGE,A. C., %~.SCHOLES,W. E. . . . . . . . . . SAVIDGE,J.,S~~MATHER,J.S.B. . . . . . . . . . . SAVKAR,S. D., Oscillations of cylindrical rods and cables in shear flows . . . SCHOLES,W. E., SALVIDGE,A. C. ANDSARGENT,J. W., Field performance of a noise barrier SCHULTZ,T. J., Diffusion in reverberation rooms . . . . . . . SCHULTZ,T. J., Sound power measurements in a reverberant room . . . . . . . . Scorr, H. L., The optimization of sound absorbers in circular ducts SEN GUPTA, G., Natural frequencies of periodic six-stringer structures using a wave approach . . . . . . . . . . . . . SHINOZUKA,M., AND YANG J.-N., Peak structural response to non-stationary random excitations . . . . . . . . . . . . . SINHA, S. C. ANDSRINIVASAN,P., A weighted mean square method of linearization in nonlinear oscillations . S~,G.C.,S~~UTLEY, W.A. : : : : : : : : : : SOVA,J.A.,S~~WILLIAMS,T.R.G.. . . . . . . . . . SRINIVASAN,P., See SINHA, S. C. . . . . . . . . . . TAM, C. K. W., On finite amplitude spinning acoustic modes and subsonic choking. . TANNA, H. K. AND MORFEY,C. L., Sound radiation from point sources in circular motion TANNA, H. K., Sound radiation from point acoustic stresses in circular motion . . UTLEY,W. A. ANDSrvrrrn, G. C., The accuracy of laboratory measurements of transmission loss (letter) . . . . . . . . . . . . . WANG, W. M., Filter design for vibration isolation between multi-resonant structures . WANG, J. T.-S., See Hsu, T.-M. WARBURTON,G.B.,S~~HENSHALL,R.D.: : : : : : : : : WELLS, R. J., Automatic data reduction with moving microphone WESTON,R. H. ANDNEWALL,A. F., Models of neural “sharpening” in the cochlea: WHY, R. G., Effects of non-linearity due to large deflections in the resonance testing of structures . . . . . . . . . . . . WKLMS, T. R. G. ANI) SOVA,J. A., Studies of fatigue damage in aluminium alloys . WOOTTEN,E. J., Instrumentation for space averaging . . . . . . . YANG, J.-N., See SHINOZUKA,M. . . . . . . . . . .
(4) 627 (3) 407 (2) 161 (4) 627 (1) 17 (1)119 (2) 189 (4) 567 (4) 505 (2) 139 (4) 643 (2) 283 (2)139 (3) 393 (3) 337 (3) 349 (4) 643 (3) 309 (4) 473 (4) 519 (1) 71 (3)443 (2) 255 (2) 283 (1) 59 (4) 505