“…3 and 5, it can be seen that the air gap is important for reducing of sound transmission in the frequency range between the ring frequency and acoustic coincidence frequency. This phenomenon is also observed when a plane wave transmits through sandwich structures [4,11,12].…”
Section: The Effect Of the Airgap On Transmissionmentioning
confidence: 67%
“…The airborne wave is the dominant wave in the UU configuration [40]. This approach proposed by Lee et al [40] has also been used by the present authors [12] for studying transmission of plane waves through infinite cylindrical shells. For brevity, the detail of this method will not be repeated here.…”
Section: Description Of Model Systemmentioning
confidence: 77%
“…L 1 , L 2 and L 3 are linear differential operators for the circular cylindrical shell which can be found in references [12,41]. Fig.…”
Section: Governing Equationsmentioning
confidence: 99%
“…Considering the equations of motion (4)-(6) and boundary conditions equation (12), the solutions for the displacement field can be expressed as…”
“…3 and 5, it can be seen that the air gap is important for reducing of sound transmission in the frequency range between the ring frequency and acoustic coincidence frequency. This phenomenon is also observed when a plane wave transmits through sandwich structures [4,11,12].…”
Section: The Effect Of the Airgap On Transmissionmentioning
confidence: 67%
“…The airborne wave is the dominant wave in the UU configuration [40]. This approach proposed by Lee et al [40] has also been used by the present authors [12] for studying transmission of plane waves through infinite cylindrical shells. For brevity, the detail of this method will not be repeated here.…”
Section: Description Of Model Systemmentioning
confidence: 77%
“…L 1 , L 2 and L 3 are linear differential operators for the circular cylindrical shell which can be found in references [12,41]. Fig.…”
Section: Governing Equationsmentioning
confidence: 99%
“…Considering the equations of motion (4)-(6) and boundary conditions equation (12), the solutions for the displacement field can be expressed as…”
“…In the analytical modelling of this problem, cylindrical shell structures need to be considered to account for aircraft fuselage geometry (e.g. [1][2][3][4][5]); the effects of external flow must be taken into account for flight conditions [1,[6][7][8][9][10][11][12]. Moreover, sound absorptive materials can be included within the sandwich core to enhance the sound insulation performance of such structures [1,[10][11][12][13][14][15].…”
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