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ELqEVIER Physica D 93 (1996) 123-136
PHYSICA
Limiting masses of solutions of the Einstein-Yang/Mills equations J,A. Smoller*" 1,2, A.G. Wasserman l
Mathematics Department, University of Michigan, Ann Arbor, M148109-1003, USA
Received 7 March 1995; revised 18 September 1995; accepted 13 November 1995 Communicated by C.K.R.T. Jones
Abstract
The first main result of this paper is that the masses of any sequence of distinct, globally defined, spherically symmetric solutions of the SU(2) Einstein-Yang/Mills equations (i.e., particle-like solutions) converge to 2. In addition, if one considers black-hole solutions of these equations, defined for r > p, where p is the radius of the black-hole (the event horizon), then it is shown that the masses of any sequence of distinct black-hole solutions converge to p + l /p if p > 1, and to 2, if p < 1.
O. Introduction
The equations of general relativity are based on
Einstein's hypotheses:
(E]) The gravitational field is a metric gij in four-
dimensional space-t ime.
(E2) At each point in space-t ime, one can diagonalize
gij as d i a g ( - I , 1, 1, 1).
(E3) The equations which determine the gravitational
field should be "covariant"; i.e., independent of
the coordinate system.
The hypothesis (El) is Einstein's brilliant insight,
whereby he "geometrizes" the gravitational field. (E2)
means that special relativity is included in general
relativity, and (E3) implies that the gravitational field
equations must be tensor equations.
* Corresponding author. E-mail: [email protected]. edu.
I Research supported in part by the N.S.E, Contract No. G-DMS-9501128.
2 Research supported in part by the ONR, Contract No. N00014-94-1-0691.
The equations of general relativity for the metric
are extremely complicated nonlinear equations, and it
is very difficult to find solutions. The first solution
found was the Schwarzschild solution [1], which is a
static (time-independent), spherically symmetric solu-
tion, where the metric is
ds 2 1
= - T - 2 ( r ) dt 2 + - - dr 2 A(r)
+ r2(d02 + sin20 dq02), (o.1)
and A(r) = (1 - 2 m / r ) = T-2(r ) . Note that when
A = 0, the metric becomes singular. This occurs at
r = 2m, and is called the "event horizon".
To incorporate an electromagnetic field into the eq-
uations, one couples Einstein's equations to Maxwel l ' s
equations, and to make the theory coordinate invari-
ant, the electromagnetic field is constructed from a
U(1) connection on a vector bundle. The resulting
Einste in/Maxwell equations admit a static spherically
symmetric solution called the Reissner-Nords t r rm
(RN) solution. Here the metric is the same form as
(0.1) above, with A (r) = (1 - ( p + , o - l ) / r + l / r 2) =
0167-2789/96/$15.00 © 1996 Elsevier Science B.V. All rights reserved SSDI 0 1 67-2789(95)0029 1 -X
124 J.A. Smoller. A.G. Wasserman/Physica D 93 (1996) 123-136
lim r(1 - A(r)). r---+ o o
The Schwarzschild solution to the Einstein equations
is also a solution to the EYM equations (when w(r ) --
1), and the mass of the Schwarzschild solution is 2m.
Similarly, the RN solution to the Einstein/Maxwell equations is also a solution to the EYM equations (when w(r ) ~ 0), and the mass is given by p + p - l .
In [7] it was proved that the masses of all particle-
like solutions are uniformly bounded. One can mod- ify that argument to show that for any fixed event
horizon p > 0, the masses of the black-hole solu- tions are also uniformly bounded. Numerical values for the first few masses were obtained in [4,7]. In this
paper we approach the problem of determining the
masses indirectly, and we obtain more precise state-
ments. We show that any sequence of distinct solu-
tions with fixed event horizon p > 0 converges to a
Reissner-Nordstrrm solution.
If (A(r) , T(r) , w(r ) ) is a solution to the EYM equa-
tions, and A(p) = 0 = At(p) for some p, then the so-
lution is called an "extreme" black-hole. (Physically,
this corresponds to zero surface temperature of the
black-hole; see [15].) The RN solution with p = 1 is
an extreme black-hole. In fact it was proved in [ l l ]
that the only extreme SU(2) static, spherically sym-
metric black-hole solution of the EYM equations is
the extreme RN solution.
The main results of this paper are (see Section 2):
(a) For fixed event horizon p, 0 < p _< 1, any se-
quence of distinct solutions of the EYM equations
converges to the extreme Reissner-Nordstr6m
(ERN) solution, uniformly on compact intervals
of the form [a, b], where a > 1. (p = 0cor re -
sponds to particle-like solutions; see [3].)
(b) For any fixed event horizon p > 1, any sequence
of distinct black-hole solutions converges to the
RN solution with event horizon p, uniformly on
compact intervals of the form [a, b], where a > p.
(c) For any sequence of distinct solutions (wn(r) ,
An (r), Tn (r)), of the EYM equations having event
horizon p >_ 0, the mass functions, p~n(r) -=
r(1 - An(r)) converge, as n ---> c~, to the mass
function of the associated RN solution. In addi-
tion the limit of the invariant quantities tZn(C~)
(the (ADM) mass) is equal to the mass of the as-
sociated RN solution.
The proofs of these results rely on an important
technical fact; namely, for any solution of the EYM
equations defined on an interval (a, b], the rotation
of the projection of the orbit in the (w-w' ) -p lane
is bounded. This result is false for intervals of the
form [a, b); see [5,9]. We pose the question: Is there a
physical interpretation of the nodal class of an EYM solution?
It is interesting to note that for essentially all so- lutions, the (ADM) mass exterior to the black-hole is less than 1/p, if p > 1, and less than ( 2 - p), if p < 1 ; see Corollary 2.5.
T -2 ( r ) , p > 1/p (see [1]). We note that A(p) --- O,
and thus p is the event horizon for the Reissner-
Nordstrrm solution. To incorporate nuclear forces, one couples the
Einstein equations to a Yang-Mills field, and to make
the theory coordinate invariant, the Yang-Mills field
is again constructed from a connection on a vector
bundle. In this paper, we consider SU(2) bundles. The
equations for static, spherically symmetric solutions
of the Einstein/Yang-Mills (EYM) equations were
first derived by Bartnik and McKinnon [3] and are
a set of three coupled ordinary differential equations
for the metric coefficients, A, T, and a connection
coefficient w (see Eqs. (1.3)-(1.5)). They discov-
ered global non-singular solutions - these are called
"particle-like" solutions. There are in fact, an infinite
family of such solutions [8].
Black-hole solutions of the EYM equations, analo-
gous to the Schwarzschild solution, were discovered
by Bizon [4], Kunzle and Masood-ul-Alam [7], and
others. In fact, for any event horizon, there are an in-
finite number of such solutions [12]; see also [14].
Associated to every particle-like, or black-hole so-
lution of the EYM equations is an invariant quantity
called the (ADM) mass; see [2]. In other words, num-
bers representing masses are a direct consequence of
the existence of such solutions, and are not prescribed
in an ad hoc manner. In the static, spherically sym-
metric case, the metric is of the form (0.1), and the
mass is (cf. [10])
J.A. Smoller, A.G. Wasserman/Physica D 93 (1996) 123-136 125
The results of this paper were announced in gr-
qc/9405003. Theorem 2.1 of this paper corrects Theo-
rem 4.1 of [9]. In [6], Breitenlohner and Maison have
shown (using different methods) that solutions con-
verge to the ERN solution in the case where p < 1.
1 . P r e l i m i n a r i e s
The EYM equations with gauge group SU(2) can
be written in the form [2]
Gij = ~ Tij, d* Fij = O, i, j = 0 . . . . . 3.
Here T/j denotes the stress--energy tensor associated
to the su(2)-valued Fang /Mi l l s curvature two-form
Fij, Gij = Rij - l Rgij is the Einstein tensor com-
puted with respect to the sought-for metric g i j , * de-
notes the Hodge star operator, and o- is a universal
constant. If we consider static, symmetric solutions,
i.e., solutions depending only on r, then we may write
the metric [3,13] as
ds 2 = - T ( r ) -2 dt 2 + A(r ) -1 dr 2
+ rZ(d02 + sin 2 0 d~b2), (1.1)
and the Yang/Mil ls curvature two-form as
F -- w ' r l d r / x dO + w'r2 d r / x (s in0 dcp)
- (1 - w2)r3 d0 /x (s in0 &p). (1.2)
Here (T, A) and w = w(r) denote the unknown metric
and connection coefficients, respectively, and r l , r2, r3
form a (suitably normalized) basis for su(2). As dis-
cussed in [3,13], the EYM equations in this framework
take the following form as a system of three ordinary
differential equations:
rAt + (1 + 2 w ' 2 ) A = 1 - ( 1 - -w2)2 / r 2, (1.3)
r2Aw '' + [r(1 - A) - (1 - w2)2/r]w '
+ w(1 - w e ) = 0, (1.4)
2 r A ( T ' / T ) = (1 -- W2)2/r 2 + (1 -- 2w'Z)A - 1.
(1.5)
T; thus we shall mainly concentrate on Eqs. (1.3) and
(1.4).
If the mass function tz(r) is defined by 3
# ( r ) = r ( l - A(r)) , (1.6)
then we require of our solutions that they have finite
(ADM) mass (cf. [2]), namely that
lira /z(r) < ~ . (1.7) r - - - + OG
In [8,12], we proved that for every p > 0,
there exists a sequence of solutions An(r) = (Wn (r), wtn (r), An (r), r) which satisfy the following:
lira A n ( r ) = 1, (1.8) F - ~ " OG
lira /~,,(r) < ~ , (1.9) J l ----~ O 0
lim (w2(r), w'( r ) ) = (1,0) . (1.10) r 1 ~ o G
Furthermore, if p > 0 , and we define the functions
4~ and u by
• (A, w, r) = r ( l - A(r)) - u2(r)/r ,
u(r) = I - w2(r),
then if A(p) = O,
~(0 , w(p), p )w ' (p) + (uw)(p) = 0: ( l . l 1)
that is, the "initial" values (w(p) , w'(p)) = (?,, ~)
must lie on the curve C(p) defined by
C(p) = {(w, w') ~ ~2: ~(0 , w, p )u / + uw = O,
w > 0, w' < 0}. (1.12)
In [12, Proposition 2.2] we proved the following local
existence result, for black hole solutions.
Proposition 1.1. For each ?, satisfying ?,2 < I, and
p q_ ?,2 5& 1 (i.e., 4~(p) 5~ 0), there exists a unique
solution (the ?'-orbit)
A(r, ?,) -~ (A(r, ?,), w(r, ?,), w'(r, ?,), r) (1.13)
of (1.3), (1.4) satisfying the initial conditions
A(p , ?,) = O, w(p, ?,) = ?,, (1.14) w'(p, •) = ~ = ~(p, ?,)
Since (1.3) and (1.4) do not involve T, we can use
these to solve for A and w, and then solve (1.5) for 3 Our mass functions are half those usually encountered in the
literature.
126 J.A. Smoller, A.G. Wasserman/Physica D 93 (1996) 123-136
defined and analytic on some interval 0 < (r - p) <
s(y). The solutions form a continuous one parameter
family (see [12, Definition 2.1]).
Next, for p > 0, we define the region F C ~4 by
f ' = {(A, w, w ~, r): W 2 < 1, A > 0,
r > p, (w, w') • (0,0)},
and we let re(y) be the smallest r > p for which the
y-orbit exits F ; re(y) = oo if the P-orbit stays in
F for all r > p. If the y-orbit exits F via A = 0,
we say that the y-orbit crashes. If O(r, y) is defined by O(r, y) = t an- l (w ' ( r , y) /w(r , y)), and - l y r <
O(p, y) < O, we set
,.Q (y ) = --(1/zr )IO (re(y ), y) -- O(p, y)];
~ ( y ) is called the rotation number (or nodal class
if (1.8) and (1.10) hold) of the y-orbit. The major result
in [12] is the following global existence theorem.
Theorem 1.2. Given any p > 0, there exists a se-
quence (Yn, fin, P) satisfying p + y~ ¢ 1 and (1.11) such that the corresponding solution A(r, Yn) of (1.3), (1.4) with these data lies in F for all r > p,
and I-2(yn) = n.
That is, for every value of the event horizon p >
0, there exists a sequence of initial values (Yn, fin) lying on the curve C (p) which yield regular black-hole
solutions having rotation number n. These solutions
have uniformly bounded masses, outside of the event
horizon [7].
Similarly, if p = 0, we proved in [8] the following
theorem.
Theorem 1.3. There exists a sequence )~n, 0 < ~-n < 2
such that the solution
A(r, ),n) = (A(r, Xn), w(r, )~n), w' (r, ~.n), rn)
of (1.3), (1.4) satisfying the initial conditions
a ( 0 , ~-n) = 1, w(0 , Xn) = 1,
w'(0, xn) = 0, w"(0, zn) = - z , , ,
£20~n) = -(1/zr)O(reO~n), kn),
where reO~n) is the smallest r > 0 for which the ~-n-
orbit exits/- ' , and
O(r, ~-n) = tan-I (w'(r,)~n)/W(r, ~n)),
with 0(0, ~-n) = 0.)
That is, there exists a sequence of"particle-like" so-
lutions having rotation number n, n --- 1,2 . . . . These
solutions have uniformly bounded masses [7].
2. L imi t ing masse s
The main results of this paper are the following:
A. Let An(r) = (wn(r), wrn(r), An(r), r) be a se- quence of distinct solutions of the EYM equa-
tions (1.3), (1.4) defined for all r > 0. Then
(i)A limn~oo An(r) : AERN(r), for each r > 1, where AERN(r) is the extreme Reissner-
Nordstr6m (ERN) solution,
AERN(r) ---- (0, 0, ((r -- 1) /r) 2, r).
(ii)A The convergence is uniform on all inter-
vals [a, b], a > 1.
(iii)A The (ADM) masses, / zn (~) , converge to 2,
the (ADM) mass of the ERN solution, as n --+
oo. Here IZn(r) = r ( l - An(r)). (iv)A The metric coefficients (An(r), Tn-Z(r)) con-
verge uniformly to the extreme Reissner-
Nordstr6m metric coefficients, (((r - 1) /r) 2,
((r - 1)/r)2), on all intervals of the form [a, oo),a > 1.
B. Let 0 < O < 1, and let An(r) = (wn(r), w'n(r), An (r), r) be a sequence of distinct black-hole solu-
tions of the EYM equations (1.3), (1.4) with fixed
event horizon p. Then p
(i)B limn-~oo An(r) = AERN(r), for each r > p, where A p is the extreme Reissner- ERN
Nordstr6m solution,
A~RN(r) = (0, 0, ((r -- 1) /r) 2, r).
lies in F for all r > 0, and satisfies £2 (;~n) = n. (Here ~(~-n) is defined by
(ii)B The convergence is uniform on all inter- vals [a, b], a > p.
J.A. Smoller, A.G. Wasserman/Physica D 93 (1996) 123-136
(iii)B The (ADM) masses,/.£ n (OO), converge to p +
1/p, the (ADM) mass of the ERN solution P
AERN, as n --~ oo.
(iv)B The metric coefficients (An (r), Tn-2(r)) con-
verge uniformly to the extreme Reissner-
NordstrOm metric coefficients (((r - 1) /r) 2,
((r - 1) / r ) 2) on all intervals of the form
[a, oo),a > p. C. Let p > I, and let An (r) = (wn (r), w~n (r), An (r),
r) be a sequence of distinct black-hole solutions
of the EYM equations (1.3), (1.4) with fixed event
horizon p. Then
(i)c l i m n ~ An(r) = A~N(r), for each r > p. (ii)c The convergence is uniform on all inter-
vals [a, b], a > p.
(iii)c The (ADM) masses,/Zn ( ~ ) , converge to p +
1/p, the (ADM) mass of the RN solution A~N,
as n -+ ~ .
(iv)¢ The metric coefficients (An (r), Tn-2(r)) con-
verge uniformly to the Reissner-NordstrOm metric coefficients ( l - ( p + p - l ) / r + l / r 2, 1 - (p + p - l ) / r + l / r2) , on all intervals of the
form [a, c~), a > p.
The proofs of these main results are given in The-
orems 2.1, 2.3, and 2.6.
Theorem 2.1. Let p > 0, and suppose that An(r) = (wn(r), W'n(r), An(r), r) is a sequence of solu- tions (1.3), (1.4), defined for all r > p, where
pA(p) = 0. Assume moreover that the rotation num-
bers S2(An) ---> ~ as n ~ o0. Then
lim A n ( r ) = { AERN(r) f o r a l l r > l i f p < l , n~o~ ARN(r) for all r > p if p > 1,
(2.1)
127
I 2 - 1/r (extreme), /ZRN(r) I p + 1 / p - 1/r (non-extreme, p > l).
(2.2)
We thus have the following corollary.
Corollary 2.2. Under the hypotheses of Theorem 2. l,
the (ADM) mass functions /Zn(r) = r ( l - An(r)) satisfy
lim #n(r ) n - - ~ O 0
2 - 1/r = p + p - 1 _ l / r
for all r > 1, if p _< 1,
for all r > p, if p > 1.
(2.3)
The convergence is uniform on compact r-intervals.
Note that from (2.1),
lim IZn(r) < /ZRN(OO) ----- / 2 i f p ~ 1, n~o~ -- | p + p- t i f p > 1,
so that the mass functions satisfy limn~oo IZn(C~) _<
/ZRN (OO). In fact, these quantities are equal, as the next
result shows.
Theorem 2.3. For any p > 0, given any sequence
An(r) = (Wn(r), w~n(r), An(r), r), of black-hole so-
lutions, (particle-like if p = 0), of (1.3), (1.4), hav-
ing unbounded rotation numbers, then the limit of the
(ADM) masses of the solutions is equal to the (ADM)
mass of the associated Reissner-NordstrOm solution;
that is
lim #n(OO) = I 2 'if p < 1, n--,oo [ p + l / p i f p > 1.
where AERN(r) is the extreme Reissner-NordstrOm
solution, AERN(r) = [0, 0, ((r -- 1) /r) 2, r], and
ARN (r) is the Reissner-NordstrOm solution, ARN (r) = [0, O, 1 -- (p + p - l ) / r + l / r 2, r]. The convergence
is uniform on compact r-intervals.
Note that the Reissner-NordstrOm mass functions 4 for black-holes are
4 See footnote 3.
(Note that this together with (2.1) implies
lim lim /z,(r)= iim lim IZn(r).) /'---~" O0 ~---~ O0 ~---Y 0~) F--')" O0
We also have the following corollary.
Corollary 2.4. Fix p > 0, and let {An(r)} be a se- quence of distinct solutions of (1.3), (1.4) defined for all r > p, where pA(p) = 0. Then (2.1) holds. In
particular, the mass functions satisfy (2.3).
128 J.A. Smoller, A.G. Wasserman/Physica D 93 (1996) 123-136
The proof of Corol lary 2.4 follows from a result
in [5], where it was shown that there are at most a finite
number of solutions of (1.3), (1.4) in each nodal class.
This implies that the rotation numbers ~ ( A n ) ~ cx~
as n ~ c~, so that the hypotheses of Theorem 2.1 are
satisfied.
Corollary 2.5. Given any e > 0 and any sequence
of black-hole solutions of (1.3), (1.4), having event
hor izon p, there are at most a finite n u m b e r of solut ions
having (ADM) mass exterior to the black-hole greater
than to- l + e, if /9 > 1, or greater than (2 - to + e), if
p < l .
Proof. If p > 1, we have from Theorem 2.3,
l im /zn(c~) =/ZRN(~x~) = p + p - l ; n- - -~ O ~
hence
1 l im (#n ( ~ ) - Un (P)) = l im (/Zn (c~) - p) = - .
If p _< 1, we have again from Theorem 2.3,
l im /Zn (c~) =/Z~RN (~X~) = 2, ?/----~ (3~
so that
l im (/Zn(C~) - tZn(p)) = l im (#n(C~) - to) n - ~ - O ~ n----~ O ~
= 2 - - p []
Before giving the proofs, we need a pre l iminary
result, which is important in its own right, and also
provides a crucial step in proving Theorem 2.1.
Theorem 2.6. If A ( r ) = (w(r ) , w1(r), A( r ) , r ) , a <
r < b, is an orbit segment in F , then l imr'~a(O(b ) -
O(r)) < cx~.
and crashes at r = a (i.e., l imr~ a A(r ) = 0), then
limr"~ a (A w I2) (r) = 0.
Remarks . It was proved in [13, Proposi t ion 5.1] that
A w I2 is bounded on all orbit segments of (1.3), (1.4)
satisfying either black-hole or particle-like initial con-
ditions. The fact that A w 12 was bounded enabled us to
show that A w ' --+ 0 at crash. This was an important
ingredient in the papers [12,13]. Lem m a 2.7 shows
that l imr ,~a(Aw12)(r) = 0 at crash if an orbit has in-
finite rotation. This s tatement is true even without the
hypothesis of infinite rotation if a > 1, and either r s a
or r"~a, but we only prove it here in the case r"~a > 1,
and the orbit has infinite rotation.
Proo f o f Lemma 2.7. Set f = Aw'2; then f satisfies
the equat ion
r Z f ÷ ( 2 r f + ~ ) W '2 + 2W(1 -- W2)W 1 = 0. (2.4)
Since the orbit has infinite rotation, it follows that
0 = l im in f r~ a f ( r ) . Now suppose lira supr '~a f ( r ) =
~r > 0; we shall show that this leads to a contradict ion
(which will prove the lemma). Choose e, with cr >
e > 0; then there exists a sequence rn~a such that
f ( r n ) = ~r - e, f l ( r n ) > O, and Iw'( r , ) [ ~ cx~ (since
[w1(rn)[ = ~/ f ( r n ) / a ( r n ) = ~/ (a - e ) / a ( r n ) , and
A(rn) ~ 0). Now for r > a we have # ( r ) = r ( l -
A ( r ) ) , so /z(a) = a, and since #1 > 0 (see [3]), it
follows that for r > a , / z ( r ) > /z(a) = a > 1. Thus if
r > a ,
(1 - w2(r)) 2 1 1 • ( r ) = I z ( r ) > a - - > a - - > 0 ;
r r a
i.e.,
q~(r) > 0 i f r > a. (2.5)
We remark that this result is false in the "forward"
direction; i.e., there are solutions of (1.3), (1.4) for
which l imr lb (O(b ) -- O(r)) = --cx~; see [5,9].
The proof of Theorem 2.6 is broken up into two
cases: a > 1 and a < 1. The case a > 1 requires a
pre l iminary lemma; namely
L e m m a 2.7. If an orbit segment A (r ) = ( w ( r ) , w ' (r ) ,
A ( r ) , r ) , 1 < a < r < b, has infinite rotation,
Thus 2 r n f ( r n ) + ~(rn) > 2(or - e). Then from (2.4)
we get the contradict ion
0 = r 2 f ' ( r n ) + ( 2 r n f ( r n ) q- clg(rn))W'(rn) 2
q- 2 ( w w ' ) ( r n ) ( 1 - w2(rn))
> r 2 f ' ( r n ) + 2 (a - ~)w'(rn) 2
+ 2 ( w w ' ) ( r n ) ( l -- wZ(rn)) > 0
for large n, since Iwt(rn)l ~ ~ . []
J.A. Smoller, A.G. Wasserman/Physica D 93 (1996) 123-136 129
W------C
, 4
W e
/ / / /
,4 '
W = l g
Fig. 1.
Proof o f Theorem 2.6. First, i f limr-~ a A(r) > 0, then
the solution extends to a - e, for some E > 0 and
hence O(r) is a cont inuous funct ion on a < r < b, so
it is bounded. Thus we may assume l imr~ a A(r) = O.
The proof is d ivided into two cases: a > 1 and a < 1.
We first assume a > 1.
We define the funct ion h(r) by
h(r) = (Aw'2)(r) + w2(2 - w2) /2r 2, (2.6)
where A, w, and w ' refer to the A-orb i t segment . Note
that h(r) > 0 for a < r < b, because A(r ) C F, and
hence A(r) > 0 and (w(r) , w ' (r ) ) :~ (0, 0). S ince
h'(r) - - 2 A w ' 4 dp w2(2 - w 2) - w '2 ( 2 . 7 )
r r r 3 '
(2.5) shows that
h'(r) < 0 i f r > a , (2.8)
and
h(b) > 0. (2.9)
We now show that the assumption that A(r ) has
infinite rotation leads to a contradict ion. Thus, un-
der this assumption, l imin f r ' ,aW2(r ) = 0, and
f rom L e m m a 2.4, l imr~a(Aw'Z)(r) = 0. Therefore
l im inf,..,., h(r) = 0, and thus for some rL, a < rl <
b, h(r j ) < h(b), and this contradicts (2.8). This
proves Theo rem 2.6 in the case a >_ 1.
We turn now to the case a < 1. This is d iv ided into
two subcases: a > 0 and a = 0. We begin with the
case a > O.
) W
Case 1: a > 0. In this case we first c la im that
l im SUpr~aClg(r ) > O. (2.10)
Thus, i f l im SUPr',a~(r) = - c 2 < O, then f rom (1.3),
which we write in the form
rA ' + 2w12A = ~ / r , (2.11)
we see that A ' = cI9/r 2 - 2 w ' 2 / 2 < ~ / r 2, so
l imsuPr \aA ' ( r ) < - c 2. Thus for r near a , r > a,
a(b) - A(r) = a ' (~) (b - r)
< lim sup A'(r) (b - a) < 0;
here ~ is in termediate to b and r. It fo l lows that
for these r , A ( r ) > A(b) > 0. On the other hand
l imr~ a A(r) = 0 < A(b), and this is a contradict ion.
Thus (2.10) holds.
N o w since a < l , a - 1/a = -2~r < 0. If we
cons ider dp(r, A, w) =-- r - rA - (1 - w2) / r , as an
abstract cont inuous funct ion o f three-variables, then
~ ( r , A, w) < r - (1 - w2)2/r , and as @(a, A,O) <
- 2 a , there exists an e > 0 such that
@ < - ~ r i f l w ] < s a n d l r - a ] < s . (2.12)
N o w cons ider the region a~ U M' where (cf. Fig. 1 )
a / = {(w, w ' ) : - s _< w _< 0, w ' > 0},
a / ' = {(w, w ' ) : 0 _< w < s, w ' < 0}.
We now cla im that
w~(r) is bounded in a~ tO ,~'. (*)
130 J.A. Smoller, A.G. Wasserman/Physica D 93 (1996) 123-136
To see this note that (2.12) implies that in the region
s~ U M ~, 4~ < -o r if Ir - al < e. The claim ( . ) now
follows from [13, Lemma 5.13].
We next show that
The orbit A ( r ) cannot stay in the region Iwl < e
for all r satisfying 0 < r - a < e. (**)
To see this, suppose that Iw(r)[ < s for all r , 0 <
r - a < s. Now for small 6 > 0, we can write
a ( a + ½e) - a ( a + 3) = a ' ( ~ ) ( ½ e - 3),
for some intermediate point ~, ~ < ~ - a < ½e. Letting
~ 0 shows A'(~) >_ 0 because limr,~ a A ( r ) = O.
Then from (2.11) we see that ~2A'(~) < q~(~). If
Iw(¢)l < e, then 4~(~) < - a so 0 < ~2A'(~) <
4,(~) < 0. This contradiction establishes (**).
Now as w' is bounded in the region ,~ U ~ ' , say
Iw'l _< M, and the orbit has infinite rotation, every
time the orbit goes through ~ /U ~l', the "time", Ar ,
it stays in ~t tO ~/' satisfies A r > e / M . Thus, as the
orbit enters ~/U ~ ' infinitely many times, it spends an
infinite t ime in ~/U ~ ' , thereby violating b - a < oo.
This contradiction completes the proof of Theorem 2.6
in the case where a > 0.
l i m s u p w ( r ) = 1 and l i m i n f w ( r ) > - 1 , (2.15) r"~0 r"~0
l i m s u p w ( r ) < 1 and l i m i n f w ( r ) = - 1 , (2.16) r "~ 0 r"~0
l i m s u p w ( r ) = 1 and l i m i n f w ( r ) = - 1 . (2.17) r ' -0 r~'0
Since (2.15) and (2.16) have similar proofs, we
shall only consider cases (2.15) and (2.17). We be-
with (2.15). Let e < 1 be chosen so small that gin
w ( r ) > - 1 + e for r near 0. Since A ( r ) >_ 0, ~ ( r ) <
r - u Z ( r ) / r , u = (1 - w2), so in the region Se =
{ w : - I + e _< w _< 1 - e}, we can find a constant
c < 0 such that
q)(r) < - c . (2.18)
Now claim that in the region Se,
( A w ' 2 ) ( r ) < 2 u 2 ( r ) / r 2.
To see this, let f = A w ~2, and set
g( r ) = r2 f (r) - 2u2(r) .
(2.19)
Since (2.13) holds, there exist null sequences rn < Sn,
such that w'(rn) = 0 = w~(Sn), and w ' ( r ) > 0 i f rn <
r < Sn. Thus we have
Case 2: a = 0. Thus suppose in this case that
lira (O(b) - O(r)) = e~; (2.13) r----~0
we will show that this leads to a contradiction.
Now if both of the following hold:
l i m s u p w ( r ) < 1 and l i m i n f w ( r ) > - 1 , (2.14) r"~0 r~'0
then there is an r / > 0 such that
lim inf(1 - w2(r)) > r/. r"~0
Then from (1.3), we obtain
r A ' ( r ) < 1 - (1 - w 2 ) 2 / r 2 < 1 - rl2/r 2,
and this implies that limr,~ 0 A ( r ) > 1. Such behavior
violates the assumption limr-~ 0 A ( r ) = 0. Thus (2.14)
cannot hold, so we are left with the following three
cases:
g(rn) < O. (2.20)
We shall show that for rn < r < Sn, and n large
g( r ) < 0 if w ( r ) ~ Se. (2.21)
Thus fix n, and let F be the first zero of g such that
Sn > F > rn, and w(F) is in the region S~. Then from
(2.4), we find,
gt(F) = (u /F) (6 -- 3w I2) -- r w ~2 + 6 u w w t. (2.22)
Now in Se, we have a bound on u from below, say
u > r / > 0. Thus for F near zero (i.e., n large), uZ/F >
r//F > 2, so f ( F ) = (Aw'Z)(F) = 2u2/F > 4. It
follows that wr2(F) > 4. Then from (2.22), we have
at F,
g'(F) < (u2/?)(6 - 3w '2) + 6w'
< ( u 2 / F ) ( - 3 t o '2) + 6w '
< - 6 w I2 + 6w' = 6 w ' ( l -- w') < O.
J.A. Smol ler , A . G . W a s s e r m a n / P h y s i c a D 93 ( 1 9 9 6 ) 1 2 3 - 1 3 6 131
Thus we have shown that g ' (7) < 0 if g(7) = 0, and
w(7) ~ Se (provided that n is large). This implies
(2.21), and hence in Se, (2.19) holds so
A w t2 < 2u2 / r 2. (2.23)
Next, if w(r ) > l / c and w ( r ) belongs to Se, then
(1.4) gives
el ) to t - - UtO C W t - - UlI) CtO j - - 1 - _> > - - > 0 ,
wt~ ( r ) r2 A r2 A r2 A
where we have used (2.18). Now on the interval
0 < w < ¼, w ~ cannot be bounded; otherwise A r =
A w / w ' ( ~ ) > constant, and (2.13) would give the
contradict ion b = e~. Thus w' > 1/c somewhere
in this interval, say at @. Then at if), w ~' > 0 and
w' cont inues to exceed 1/c, so w 't > 0. Thus in
the region S~, for w > tb, w ~ is increasing, so w t is
increasing from w - ¼ to w = 1 - e. Furthermore,
w' cannot be bounded in any region on which the
orbit goes through infinitely often; otherwise we can
again bound A r from below by a positive constant. In
part icular w'(r l /4) ~ oc as the orbit rotates (where
w(r l /4) = ¼) and so w' must tend to infinity in the
region ¼ < w < 1 - e. Thus we may assume that r
is so close to zero that in the region } < w < 1 - e,
- u w > ~ w ' . (2.24)
Now from (1.4), if ¼ < w _< 1 - e, (2.22) and (2.24)
give
But as w~(rt/4) ~ ~ , we see that we have a contra-
diction. This contradict ion shows that (2.15) cannot
occur. (As we have remarked above, a similar proof
shows that (2.16) cannot occur.)
Now suppose that (2.17) holds. We begin by proving
that, i f w ' > 0 , a n d - I < w _ < 0 ,
(Aw'2) ( r ) < u 2 / r 2 + 2; (2.25)
(cf. (2.19)). To see this, again write f = A w '2, and
let us change the g from the proof of (2.21) to
~(r) = r 2 f - u 2 - 2r 2.
Now when w' = 0 , ~ < 0. As in the last case, we
show that ~(F) = 0 implies ~ '(~) < 0, so ~ is always
negative. We have, in the region w' > 0, - 1 < w < 0,
~ ' (7) = 2 F f - ( 2 F f + ~ ) t o t 2 - 2 u w w '
+ 4 u w w t - 47
= 2 7 f ( 1 - w ' 2 ) - 7 w '2 + r A w '2
-t- ( u 2 / r ) w '2 q - 2uww' - 4 7
= T w ' 2 ( 2 A - 2 A w '2 - I + A + u2 /F 2)
+ 2 u w w ~ - 47
= 7wtZ(3A - 1 - 2u2 /~ 2 - 4 + ?i2/72)
+ 2 u w w ' - 47
= T w ' Z ( 3 A - 5 - - ~t-2/72) + 2UWW' -- 47 < 0,
• w' - u w - 0 . 9 q ~ w t - 0 . 9 ~ w t2 It 1/)1 1/) - - ~> - -
r2 A - r2 A r2 A w t2
- 0 . 9 q ~ w I2 > W t" - 2u 2
But in this region ¢' < - c (by (2.18)), and u 2 < 1.
Thus we obtain
w t' > k w t3 if 1 < w < 1 - e.
Then integrat ing the inequal i ty w " / w t2 > k w ' from
rl/4 to r l -E ( w ( r i - E ) = 1 - e), we get
1 1 1
wt(r l /4) -- wt(r l /4) w t ( r l - e )
> k ( l - e - 1 ) _ ~ > 0 .
and this proves (2.25).
Now i f 0 < E < ¼, let T~ = { ( w , w ' ) : - l + c <
w < 0, w ' > 0}. In Te, we again have a bound on 4~
of the form (2.18). Moreover, as above, w' cannot be
bounded on - 1 + e _< w < - 3, and if w' > 1/c, w" >
0. We can thus assume that wt(r_3/4) ~ cx3 as the 3 orbit rotates through this region; (w(r -3 /4 ) ---- - ~ ) .
Furthermore, if r is sufficiently small, a bound of the 3 form (2.24) holds in Te. Then from (1.4), on - ~ _<
w < O . w ' > O ,
- -0 .9@w' --0.94~w '3 - 0 . 9 4 ~ w ~3 l/3/f > - - >
r2A r 2 A w r2 u 2 + r 2
- 0 . 9 4 ~ w ~ > >_ k w p3, - - 7 2
132 J.A. Smoller, A.G. Wasserman/Physica D 93 (1996) 123-136
where k > 0 is a constant. Thus tOrt/tO t2 > kw' , and
integrating this from r_3/4 to ro (here w(ro) = 0), we
get
1 , 1 > - - + > k ,
wt(r-3/4) -- wt(ro) w'(r-3/4) --
and as w~(r_3/4) ~ cx~, we obtain the desired con-
tradiction. This proves that (2.17) cannot occur, and
completes the proof of Theorem 2.6. []
Proof o f Theorem 2.1. Fix p >_ 0, and R > max(l , p).
Now from [13, Lemma 4.2], there exists an r / = r/(R)
such that for all n,
1 > An(R) > rl.
Now consider the sequence of points
!
A n ( R ) = (wn(R) ,Wn(R) ,An(R) ,R) , n = 1 , 2 ; . . .
From [12, Proposition 2.5], there exists a r > 0, such
that IW'n(R)[ < r, for all n. Since w2(R) < 1, the
sequence { An (R) } contains a convergent subsequence
An~(R) ~ P =-- ( ~ , ~ , A, R),
where ~ 2 < 1, [~t[ < r, and A > r/.
We now show that
e = (0, 0, A, R). (2.26)
To see this, we first show that P ¢ F . Suppose that
P E F , and let A(r ) = (w(r), wl(r), A(r), r) be the
unique orbit through P. It then follows as in the proof
of Theorem 4.1 in [12], that the orbit A(r ) can be
continued back for r > p and has unbounded rotation;
this contradicts Theorem 2.6. Thus P ¢ F , i.e., either P = (4-1,0, A, R) or P = (0, 0, A, R).
Now in order to prove (2.26), we shall show that
numbers m, 3, and w0, 0 < w0 < 1 (all independent of n) such that if w 2 < w(r) 2 < 1, then
a( r ) >_ ~ and Iw'(r)[ _< m. (2.29)
Thus, since the An-orbits are connecting orbits, we
may assume, without loss of generality, that for Ank -
orbit, we have
?
lira (Wnk(r), Wnk(r), Ank(r)) = (1, 0, 1). r ---~ o o
Let rk denote the largest r for which Wnk (rk) = wO.
Now consider the points
Qk = (wo, Wlnk (rl~), Ank (rk), rk).
Since rk < R for each k, it follows from (2.29) that
the sequence Qk has a convergent subsequence which
converges to a point
Q = (w0, w6, Ao, r0),
where [w6l _< m, and A0 _> 3; thus Q 6 F . Then by
considering the backwards orbit through Q (defined
for r < r0), we obtain the same contradiction to The-
orem 2.6 as before; i.e., as above, the backwards orbit
through Q, defined for r < ro, would have infinite
rotation, and crashes at r = p. It follows that (2.26)
holds; thus
Ank (R) ~ (0, O, A, R).
We next calculate A. To do this, we note that as
A > 0, solutions through (0, 0, A, R) are unique. But
the Reissner-Nordstr6m solution
w(r) -= 0, A(r) = 1 - c / r -4- 1/r 2 (2.30)
satisfies (1.3) and (1.4). Hence it is the unique solu-
tion through (0, 0, A, R). Here c is determined by the equation 1 - c / R + 1 /R 2 = -A.
We shall now verify some claims about this solution.
D
P ~ ( - t - I ,O ,A ,R ) . (2.27) Claim1. c 2 ~ 4.
Indeed, suppose that
e = (1,0, A, R) (2.28)
(the proof in the symmetric case is similar). We recall from [8] that if w 2 is near 1 then w' is bounded, and
A is bounded away from zero. That is, there exist
Proof If C 2 < 4, then A(r) > 0 for all r, and we
can find an rl, 0 < rl < R, such that A(rl) > 1; cf. Fig. 2. Thus since lim Ank (R) = A(R) , it follows
by "continuous dependence on initial conditions", that
Ank(rl) --+ A(rl) . Since Ank(rl) ~ A(rl) > 1, we get a contradiction. []
J.A. Smoller, A.G. Wasserman/Physica D 93 (1996) 123-136 133
1 .....................
{
r I R
A(r')
Proof If A(r) has a single root, then ¢2 = 4 so by
Claim 2, c = 2 and thus A(r) = ( ( r - l ) / r )2 ; cf.
Fig. 3. In this case, Ank(R) --+ A ( R ) so Ank(P)
A(p) . This implies Ank(P) --~ A(p) , which is impos-
sible since Ank (P) = 0 but A(p) > O. []
) r Thus A(r) has two roots, 0 and 0 -~, where 0 >
l > 0-1', cf. Fig. 4.
Fig. 2. c 2 < 4. Claim 4. 0 = p.
1 .....................
l p R
) r"
Fig. 3. c 2 = 4 .
Remark. To invoke "continuous dependence on initial
conditions", we must have A(r) > 0 on rl < r < R.
Claim 2. c > O.
Proof Otherwise A(r) > 0 if r > 0 and we get a
similar contradiction as in Claim 1. []
Proof I f p > 0 , t h e n A ( r ) > 0 o n p < r < R. Then
by "continuous dependence", lim Ank (/9) = A(p), and
this gives the same contradiction as in Claim 3. Thus
p < 0. Suppose p < 0; we will show that this is im-
possible. Thus, if p < 0, then for each r 6 [0, R],
there is an r/(r) > 0 such that An~(r) > r/(r); this fol-
lows from [9, Lemma 4.2], where, it is easy to check
that o(r) is a continuous function of r. Thus, by com-
pactness, we can find an ~ > 0, independent of k,
such that Ank(r) > -~ if 0 < r < R. Since A(O) =
O, A(O + e) < ~ for small e > 0. By "continuous de-
pendence" on the interval 0 ÷ e < r < R, we obtain
the contradiction
< limAnk(O + e ) = A(O + e ) < ~;
thus p = 0. []
We now consider separately the cases p > 1 and p < l .
Case 1. p > 1.
Claim 3. A(r) = 0 has two roots.
It follows from Claim 4, that if p > 1, c = p + 1//9,
and so c does not depend on the subsequence chosen.
This implies that the entire sequence {An(R)} con-
verges to (0, 0, A, R), where A is uniquely determined
by the equation A = 1 - (p ÷ p I ) / R ÷ R -2. Thus
A(r) = l - ( p + 1 / p ) / r + l / r 2 s o i f r > p, An(r) --+
1 ..............
1 r R 1
A(r)
) 1"
Fig. 4.
134 J.A. Smoller, A.G. Wasserman/Physica D 93 (1996) 123-136
A(r) , or 1 - IZn(r)/r -+ 1 - (p + 1 / p ) / r + 1/r 2, so
lZn(r) --+ (p + I / p ) - 1 /r . This proves (4.1) in the
case p > 1. We now consider
Case 2. p < 1.
Claim 5. A(r ) = 0 has one root; i.e., c = 2.
Proof. Suppose A(r) had two roots 0 - l , 0 . 0 > 1 >
0 -1 ; cf. Fig. 4. Then R > 0 is impossible because as
above, we can choose small E > 0, and using 0 + E
we obtain contradiction as in Claim 4; thus R < 0.
Now as p < 1, and we are considering only those r
for which r > p, we have A ( R ) < 0, but Ank(R) >
0 > 0; this contradiction implies that R < 0 is also
impossible. []
Thus if p _< 1, A(r) = ((r - 1) / r )2; as in Case 1,
this representation shows that the entire sequence
{An(R)} converges to (0, 0, A, R). Now if r > 1,
An(r) -+ A(r ) so 1 - I-tn(r)/r ---> 1 - 2 / r + 1/r 2, or
tXn(r) ---> 2 - 1 /r . This proves (2.1) in the case p _%< 1.
To complete the proof of Theorem 2.1, we must
show that the convergence in (2.1) is uniform
on compact r-intervals. Thus let 1 = [ a ,b ] C
(max(p, 1), c¢). Then using the fact that A(r) > 0 on
I , if the An-orbits converge to the A-orbi t at a point
in I , it follows again by "continuous dependence
on initial conditions", that. the An-orbits converge
uniformly to the A-orbi t on the entire interval. In
particular An(r) ---> A(r ) uniformly for r c I . Thus
#n ( r ) ~ # ( r ) uniformly on I . This completes the
proof of Theorem 2.1. []
We can now turn to the proof of Theorem 2.3. We
begin with the following lemma.
Lemma 2.8. There exist positive numbers M and R,
both independent of n, such that
[ r W ' n ( r ) l < M i f r > R . (2.31)
Proof From (1.4), we obtain
( ~ ) w( l - w 2 ) (rw' ) ' = w' 1 - - ~ r a '
so at a critical point for rw' ,
w(1 - W 2) rw ' -- (2.32)
A(1 - ~ / r A )
Now from a result in [7] (done for particle-like so-
lutions, but easily extended to black-hole solutions),
there exists a number M1 > 0 (independent of n, but
depending on p), such that for every r > 0, #n (r) _<
M1; then ~n(r ) < M1, for every r > 0. Thus we can
find a 3 > 0 such that
An(r) = 1 - t xn(r ) / r >_ 1 - M 1 / r > 6
if r is sufficiently large, and thus for such r ,
qbn/rAn < M l / r 6 ,
s o
1 -- ~ n / r A n > 1 - M1/r8 > 1,
i f r is sufficiently large, say r > R > max( l , p). Thus
at a critical point for rw' , (2.31) implies
, wn( l - w n) 2 rWn(r) < < - i f r > R. (2.33)
I An(r )
Now from [12, Lemma 4.1], r w ' ( r ) ~ 0 as r
o0. Moreover, since (wn(R) , w'n(R)) --+ (0, 0) (proof
of Theorem 2.1) we see that we can find a constant
M2 > 0 such that I R w ' ( R ) I < M2 for all n. This
together with (2.33) shows that (2.31) holds with M =
max(M2, 2/3). []
We can now complete the proof of Theorem 2.3.
For some constant c > 0, and R > R we have
O0 - / # n ( O 0 ) -- l z n ( R ) = # t n ( r ) d r
-fi
(1 - - 1/)2) 2 = ( 2 A n w ~ + rT ) d r
o o
dr c <_c
Also ~RN(R) -- ~,RN(e~) = - -1 /R . Now let e > 0
be given. Choose R > R such that (1 + c ) / R < e/2 .
J.A. Smoller, A.G. Wasserman/Physica D 93 (1996) 123-136 135
For this R, choose N so large that n > N implies that
I#n(R) - #RN(R)[ < e/2; this can be done because
of Theorem 2.1. Then n > N implies
I/zn (ec) - / Z R N ( O O ) < [/Zn ((3~) - - ~ n ( ' e ) [
+ I#n(e) -/ZRN(R)I
+ I#RN(R) -- #RN(C~)I C e 1
< = + + : < e . R 2 R
This completes the proof of Theorem 2.3. []
lZn(r) >/Zn(rl) > /ZRN(rl) -- e /2
> #RN(OO) -- ~" > /ZRN(r) -- 6.
Thus, if r > rl and n > max(Ni, N2),
[/Zn(r) --/ZRN(r)l < ~,
so the functions {#n(r)} converge uniformly
[rl, oe). Then if r >_ rl and n >_ max(Ni, N2),
[An(r) - ARN(r)I _< (l/r)llzn(r) -- #RN(r)[
<_ (1/rl)[#~(r) --/ZRN(r)l,
o n
To complete the proofs of the main results A, B, and
C, above, we must show that the metric coefficients
An and Tn converge to AERN if 0 < p < 1, or to
A~N if p > 1, uniformly on an interval [a, ~ ) , where
a > max(p, 1).
We begin with the Ans. To prove the uniform con-
vergence of the Ans, we shall first show that the mass
functions #n (r) = r (I - An (r)) converge uniformly.
Let e > 0 be given, and let /ZRN(OO) denote either
the mass of the ERN solution or the RN solution with
event horizon p.
From (iii)A or (iii)B or (iii)c, we can find N1 such
that for n > NI
]An(OO ) - - /ZRN(OO ) < e/2.
Since/z ' > 0~/zn (r) < / zn (~x~), so
and this implies that the Ans converge uniformly on
[rl, ~x~). Now in [12] we have shown that for each n,
Tn-2(r) : An (r) exp(2 Qn (r)), (2.36)
where Q~ = 2w'n2/r. Thus, in order to show that Tn -2
coverges to ARN uniformly on an interval [a, cx~), a >
max(p, 1), it suffices to show that {Qn (r)} converges
uniformly to 0 on such an interval.
Now we normalize T,, so that T,, (c~) = 1, for each
n, and as An(cX~) : !, (2.36) requires Qn(oo) = 0.
Then
Qn(r) = - ~l 2w'2(s)- ds. J S F
But using (2.31), we see that i f r > max(rl , R) = r2,
we have
#n(r) < #RN(OC) + e/2.
We can find rl > max(p, 1), such that
/ZRN(OO) --/ZRN(rl) < e/2, (2.34)
because ~RN is continuous. Then if r > rl ,
/ZRN(O0) -- /ZRN(r) < /ZRN(OO) -- /ZRN(rl) < e/2,
SO if r _> r I and n > Ni,
oo
I Qn(r)l _< j s3 ds = = r---T-,
F
SO Qn(r) ~ O, uniformly on an interval of the form
[a, c~). This completes the proof.
Finally, we remark that there is no uniform conver-
gence of the connection coefficients wn on any inter-
val [a, c~), since for each n, w2(r) --+ 1 as r ~ cx~,
while WRN(r) = 0 for every r > 0.
IZn(r) < /ZRN((X0 %- e /2 < /ZRN(r) -I- E. (2.35)
On the other hand, because of Theorem 2.1, we can
find N2 such that n > N2 implies
/Zn(rl) > /ZRN(rl) -- ~/2.
Thus, if n > N2 and r > r l , using (2.34), we get
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