Development and validation of preliminary analytical models for aircraft interior noise prediction
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[1] R. Vaicaitis. Noise transmission by viscoelastic sandwich panels , 1977 .
[2] W. H. Mayes,et al. Interior noise levels of two propeller driven light aircraft , 1975 .
[3] Leslie Robert Koval,et al. Effect of air flow, panel curvature, and internal pressurization on field‐incidence transmission loss , 1976 .
[4] R. Plunkett,et al. Formulas for Stress and Strain , 1965 .
[5] J. F. Wilby,et al. Band-limited power flow into enclosures , 1977 .
[6] John F Wilby,et al. THE RESPONSE OF SIMPLE PANELS TO TURBULENT BOUNDARY LAYER EXCITATION , 1967 .
[7] Rimas Vaicaitis,et al. Investigation of Interior Noise in a Twin-Engine Light Aircraft , 1978 .
[8] J. T. Howlett,et al. Measurement, analysis, and prediction of aircraft interior noise , 1976 .
[9] N. Mclachlan. Bessel functions for engineers , 1934 .
[10] irwin Guttman,et al. Introductory Engineering Statistics , 1965 .
[11] R. W. White. Predicted vibration responses of Apollo structure and effects of pressure correlation lengths on response , 1968 .
[12] Leslie Robert Koval,et al. On sound transmission into a thin cylindrical shell under “flight conditions” , 1976 .
[13] A. H. Marsh,et al. Interior noise control prediction study for high-speed propeller-driven aircraft , 1979 .
[14] Leslie Robert Koval,et al. Effects of cavity resonances on sound transmission into a thin cylindrical shell. [noise reduction in aircraft fuselage] , 1978 .