The bending stresses from Reference 3 are (77) (78) (79) is the distance from the centerline in the vertical axis References E. Richards & D. Mead, Noise and Acoustic Fatigue in Aeronautics, Wiley, New York, 1968. T. Irvine, Natural Frequencies of Rectangular Plate Bending Modes, Revision B, Vibrationdata, 2011. J.S. Rao, Dynamics of Plates, Narosa, New 1999. D. Segalman, C. Flucher, G. R Field; An Efficient Method for Calculating RMS von Mises Stress in a Random Vibration Environment, Sandia Report: SAND98-0260, UC-705, 1998. T. Irvine, Steady-State Vibration Response of a Plate Simply-Supported on All Sides Subjected to a Uniform Pressure, Revision C, Vibrationdata, 2014. APPENDIX A
The bending stresses from Reference 3 are (77) (78) (79) is the distance from the centerline in the vertical axis References E. Richards & D. Mead, Noise and Acoustic Fatigue in Aeronautics, Wiley, New York, 1968. T. Irvine, Natural Frequencies of Rectangular Plate Bending Modes, Revision B, Vibrationdata, 2011. J.S. Rao, Dynamics of Plates, Narosa, New 1999. D. Segalman, C. Flucher, G. R Field; An Efficient Method for Calculating RMS von Mises Stress in a Random Vibration Environment, Sandia Report: SAND98-0260, UC-705, 1998. T. Irvine, Steady-State Vibration Response of a Plate Simply-Supported on All Sides Subjected to a Uniform Pressure, Revision C, Vibrationdata, 2014. APPENDIX A
ss_plate_oblique_incidence_revF.docx