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Structural Acoustics:A General Form of Reciprocity
Principles in Acoustics
K. Case
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Structural Acoustics: A General Form of Reciprocity Principlesin Acoustics
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K. Case
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13. ABSTRACT (Wasmum 200 wore)
A generalized Reciprocity Principle for Acoustics is obtained. By specialization,various principles which appear in the literature are obtained.
14. SUIMECT TERnS IS. NUMBER Of PAGES
Rayleigh, mass conservation equation, green's thereom t6. PIKE coot
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UNCLASSIFIED UNCLASSIFIED UNCLASSIFIED SARNSN 7140Q-1-290-S500 Stamdard Form 296 (Rev 2-69)
Ž6ro t AN % M
Abstract
A generalized Reciprocity Principle for Acoustics is obtained. By spe-
cialization, various principles which appear in the literature are obtained.
1l.,
1 INTRODUCTION
According to reference [1], Russian measurements on the acoustic re-
sponse of submarines to internal and external excitation make extensive use
of the "Reciprocity Principle." While this can hardly be anything but an
application of Green's theorem, the way the theorem is stated seems to be
slightly different than that in the usu l literature - and no derivation is
given. Accordingly, it may b, useful to see what forms of a "Reciprocity
Principle" one might have.
The standard literature is a little vague. Rayleigh's [2] form relates the
pressure at a point B due to a source at A to the pressure at A with the same
source at B. The derivation assumes a bounded region with rigid boundaries.
It is indicated that the results hold for an infinite region with rigid finite
boundaries and a radiation condition at infinity.
Landau and Lifshitz [3]' discuss only an infinite region with no finite
boundaries. The statement is the same as Rayleigh but there is a generaliza-
tion to inhomogeneous media. Addition [3]b there is a problem given which
relates velocities due to dipole sources. Morse and Ingard [41 give the same
result as Rayleigh but for both rigid and compliant boundary conditins.
The result implied in [1] seems to relate the pressure at A due to a localized
force at B to the velocity at B due to a mass source at A.
Below we give a very general relation which requires only an impedance
type boundary condition on finite boundaries. By specializing, we immedi-
ately obtain the three kinds of reciprocity principles discussed above. Clearly
other specializations will yield additional principles. We leave it to the reader
to determine these - and their usefulness.
2
2 BASIC EQUATIONS
These are:
a) The Euler Equation
P{l+a(V v)V} =-VP
b) The Mass Conservation Equation
ap5t+V.pfy=O
c) An Equation of State
P = P(p).
For acoustics we linearize putting
P - Po + P'i, = 'o + f"'.
Here, as compared to Landau and Lifshitz [3), we choose the homogeneous
case p. = constant and i0 = 0. The linearized equations are (after dropping
the primes)
Po 7j = -VPopa-+poV-v = 0.
N--" = '9" The resulting equations are
Po-: = -VP
3
1 oP2- t6ý-- + P0 v . 0.
Assuming simple harmonic motion, i.e., all quantities - e-iw' yields.
-iwpot3 = -VP
-p+ po V 6 = 0.C2 .
Let us introduce forcing terms into both equations. Then
- iwpo0 = -VP + P(i - f1 ) (2-1)
-iWP + poV . I = M(f - ý2 ). (2-2)
Eliminating 5 we obtain
(V 2 + k 2)p = V. P + iwM, (2-3)
where k2 = W3/C2.
We want to put this in a form to apply Green's Theorem. We con-
sider pressures P1 (corresponding to an FI, M1) and P2 (corresponding to a
F2, M2). Thus, we have
(V'2 + k2)P 1(F') = V' F1(i' - •) + iwM1 (i' - i) (2-4)
(V' + k 2)P2(,') = V' .• 2(f' - D) + iwM2 .(#' - F2 ) (2-5)
Multiply Equation (2-4) by P2(i') and Equation (2-5) by P1 (iý'). Sub-
tract and integrate over the fluid. The result is:
Jd3i (P 2( I')V* P&') - P-I-)V'2P2fP)}
4
= d3r' {P,(F')V'.(' - I) + iWP 2 (f')MI(i:' - r)} (2-6)
- fd3r' {Pi(P')V'. -( ) + iwP&(2')M 2(' - r 2)}
Using Green's Theorem and assuming impedance boundary conditions
(i.e. P and RP-- are proportional on the boundary) we see that the left side of
Equation (2-7) is zero.
Thus
f d r'{P2(P')V'. • (?' - f') + iwP2(ý')Mi(F' - ri)}
= ,d3r' {IP(F')V'. •(F' - •)j + iwP,(P')M2(P'- r2)}. (2-7)
This is our general reciprocity principle. Specializing the Ps and Ms
will give the specific principles mentioned in the introduction.
5
3 SPECIAL CASES
Here we will only consider the situation when the Fs and Ms are con-
stants time 6 functions. To keep things straight, it is convenient to introduce
a special notation. Thus
P1 which corresponds to f'(• - i ) equal to F16(f - ') (PA now
a constant vector) and M1 (- - i1) equal to Mb(9 - 72) will be
denoted as
a) Let P, = 2 =O.
M, (f' f,) --- M6(f,'- fa
M2(f -r2) M~' 2
(M a constant).
Then Equation (2-7) reads
P(P" = 0M, Ul,; 2) = P(F = 0, M, 2; fi). (3-1)
Since both sides are proportional to M, we can take this equal to 1 and
Equation (3-1) is the statement that
P(FI; f 2) = P(f2; ý1). (3-2)
7
This is the standard Rayleigh form of the reciprocity principle. In
words: the pressure at ij due to a unit source at i 2 is the same as the
pressure at f 2 due to a unit source at f.
b) Let M1 = M2 = 0.
FA(fi'-) = 2b(fr ý
Equation (2-7) becomes
P1 - V'iP (P2, ';i~ f 2I V' P (P1F'i;i (3-3)
Since the gradients are proportional to the velocities we can rewrite
Equation ( 3-3) as
FP, .(P 2 ,,f';,)= f vP, b (P,r;r') (3-4)
Now both sides are proportional to the magnitudes of both F1 and F2 .
We can then choose both to be of magnitude 1. We choose -P and A 2
separately to be 1 of 3 orthogonal unit vectors el, e2, e3 . This yields
the relations
ý&j(ei, f'; r') "- ýj(ii,r, f ' (3 -- 5)
(i = 1,2,3).
Thus the velocity is the ith direction at r, due to a force in the ith
direction at i' is the same as the velocity in the ith direction at r. due
to a force in the ith direction at ,'1 .
If we choose P, and P2 orthogonal, we get the 6 relations
ý (Zj, f', , ) = iiA(,,,'; i) (3-6)
8
i j.
Thus the velocity in the ith direction at f' due to a force in the jth
direction at €2 is equal to the velocity in the jth direction at F' due to
a force in the ith direction at fl'.
c) LetF1 = 0, M1 = Mb(F'- f1 ),
F2 = P26( -r 2 ), M2 0.
Then P&(i') = P(FP = 0, M, f 2; f')
P2 = P(F2,0, F2
Equation (2-7) becomes (on replacing pressure gradients by velocities)
iwMP(P2,0, r';iF) =- F2 "( =,iwpo
Since both sides are - M and (P 2), we can take M = 1, and P 2 = e, where i
- 1, 2, 3 yields 3 orthogonal unit vectors.
Here we have the three relations
w2poP(li,0,r';f1)=vi(FI = 0,1,ý,;if) i= 1,2,3 (3-7)
In other words this says: The pressure at i, due to a force at F' in the ji
direction is proportional to the velocity in the ith direction due to a source
at r, at F2.
We hazard the guess that this is the reciprocity principle referred to in
reference [1].
9
References
[1] Donskoy D., 1991 "Soviet R&D in Low-Frequency Underwater Acous-
tics," published by Delphic Associates Inc., 7700 Leesburg Pike, No.
250, Falls Church, Va 22043 .
[2] Rayleigh, J. W. S., 1945, "The Theory of Sound", Vol II, p. 145, Dover
Publications, NY.
[3) Landau, L. D. and E. M. Lifshitz, 1959, "Fluid Mechanics," Pergamon
Press.
a) No. 74
b) Problem on p.291
[4] Morse, P. M. and K. U. Ingrad,(1986), "Theoretical Acoustics", Prince-
ton University Press, Princeton, NJ, p. 134 , 312, 320, 342, 405 (1986).
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