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can be applied.

      1.7.2 Response of MIMO Systems to Random Load

      When the input can only be defined by a cross spectral matrix [Sff], the same is true for the response Gm(ω).

       Start 1 By 1 Matrix 1st Row bold-italic upper S Subscript g g Baseline EndMatrix equals upper E left-bracket Start 1 By 1 Matrix 1st Row bold-italic upper G EndMatrix Superscript asterisk Baseline Start 1 By 1 Matrix 1st Row bold-italic upper G EndMatrix Superscript upper T Baseline right-bracket (1.205)

      with

StartLayout 1st Row 1st Column Start 1 By 1 Matrix 1st Row bold-italic upper G Superscript asterisk Baseline left-parenthesis omega right-parenthesis EndMatrix 2nd Column equals Start 1 By 1 Matrix 1st Row bold-italic upper H Superscript asterisk Baseline left-parenthesis omega right-parenthesis EndMatrix Start 1 By 1 Matrix 1st Row bold-italic upper F Superscript asterisk Baseline left-parenthesis omega right-parenthesis EndMatrix 3rd Column Start 1 By 1 Matrix 1st Row bold-italic upper G left-parenthesis omega right-parenthesis EndMatrix Superscript upper T 4th Column equals Start 1 By 1 Matrix 1st Row bold-italic upper F left-parenthesis omega right-parenthesis EndMatrix Superscript upper T Baseline Start 1 By 1 Matrix 1st Row bold-italic upper H left-parenthesis omega right-parenthesis EndMatrix Superscript upper T EndLayout

      and so

       Start 1 By 1 Matrix 1st Row bold-italic upper S Subscript g g Baseline EndMatrix equals upper E left-bracket Start 1 By 1 Matrix 1st Row bold-italic upper H Superscript asterisk Baseline EndMatrix Start 1 By 1 Matrix 1st Row bold-italic upper F Superscript asterisk Baseline EndMatrix left-parenthesis Start 1 By 1 Matrix 1st Row bold-italic upper H EndMatrix Start 1 By 1 Matrix 1st Row bold-italic upper F EndMatrix right-parenthesis Superscript upper T Baseline right-bracket equals upper E left-bracket Start 1 By 1 Matrix 1st Row bold-italic upper H Superscript asterisk Baseline EndMatrix Start 1 By 1 Matrix 1st Row bold-italic upper F Superscript asterisk Baseline EndMatrix Start 1 By 1 Matrix 1st Row bold-italic upper F EndMatrix Superscript upper T Baseline Start 1 By 1 Matrix 1st Row bold-italic upper H EndMatrix Superscript upper T Baseline right-bracket (1.206)

      The system matrix H can be removed from the expected value operator

       Start 1 By 1 Matrix 1st Row bold-italic upper S Subscript g g Baseline EndMatrix equals Start 1 By 1 Matrix 1st Row bold-italic upper H Superscript asterisk Baseline EndMatrix upper E left-bracket Start 1 By 1 Matrix 1st Row bold-italic upper F Superscript asterisk Baseline EndMatrix Start 1 By 1 Matrix 1st Row bold-italic upper F EndMatrix Superscript upper T Baseline right-bracket Start 1 By 1 Matrix 1st Row bold-italic upper H EndMatrix Superscript upper T (1.207)

      and finally

       Start 1 By 1 Matrix 1st Row bold-italic upper S Subscript g g Superscript asterisk Baseline EndMatrix equals Start 1 By 1 Matrix 1st Row bold-italic upper H EndMatrix Start 1 By 1 Matrix 1st Row bold-italic upper S Subscript f f Superscript asterisk Baseline EndMatrix Start 1 By 1 Matrix 1st Row bold-italic upper H EndMatrix Superscript upper H (1.209)

      Bibliography

      1 Julius S. Bendat and Allan G. Piersol. Engineering Applications of Correlation and Spectral Analysis. Wiley, New York, 1980. ISBN 978-0-471-05887-8.

      2 Cyril M. Harris and Charles E. Crede. Shock and Vibration Handbook. McGraw-Hill, New York, NY, U.S.A., second edition, 1976. ISBN 0-07-026799-5.

      3 P. A. Nelson and S. J. Elliott. Active Control of Sound. Academic, London, 1993. ISBN 0-12-515426-7.

      Notes

      1 1 In this book the convention ejωt for the complex harmonic function is used. Literature that deals with wave propagation often use e−jωt to have positive wavenumber for positive wave propagation. However, as in every textbook in acoustics I denote the used convention on the first page to avoid confusion.

      2.1 Introduction

      The acoustic wave motion is described by the equations of aerodynamics that are linearized because of the small fluctuations that occur in acoustic waves compared to the static state variables. The fluid motion is described generally by three equations:

       Continuity equation – conservation of mass

       Newton’s law – conservation of momentum

       State law – pressure volume relationship.

      For lumped systems the velocity is simply the time derivative of the point mass position in space. The same approach can be used in fluid dynamics, but here the continuous fluid is subdivided into several cells and their movement is described by trajectories. This is called the Lagrange description of fluid dynamics. Even if the equation of motions are simpler in that formulation it is quite complicated to follow all coordinates of fluid volumes in a complex flow. Thus, the Euler description of fluid dynamics is used. In this description the conservation equations are performed for a control volume that is fixed in space and the flow passes through this volume.

      In this chapter, the three dimensional space is given by the Cartesian coordinates x={x,y,z}T and the velocity of the fluid v={ vx, vy, vz }T.

      2.2 Wave Equation for Fluids

      2.2.1 Conservation of Mass

      1 The elemental mass m=ρdV=ρA with A=dydz.

      2 Mass flow into the volume (ρvxA)x.

      3 Mass flow out of the volume (ρvxA)x+dx.

      4 Mass input from external sources m˙.

      leading to equation

       StartFraction partial-differential left-parenthesis rho upper A d x right-parenthesis Over partial-differential t EndFraction equals left-parenthesis rho v Subscript normal x Baseline upper A right-parenthesis Subscript x Baseline minus left-parenthesis 
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