The swirling, radial free jet in the presence of a transverse magnetic field

4
Vol. 17, 1966 Kurze Mitteilungen - Brief Reports - Communications br~ves 639 Then, 0 = aij tij = 2 6 (4 + ~2)-1/2 (tll _ t22 _ ~ t12) + 2 [2+ 1 2 (1 1 \1121-11~[t13 { 1 (1 1 \1/2'/231 1 ~(1+ 1 1/2 -1/2 { 1 --(1 1 } t23] , and since ,~, e, /, are completely arbitrary we obtain RIVLIN'S universal relation tll-- t2. 2 = ~t12, together with tla : t~3 = 0 . 5. Concluding Remarks We have dealt here with universal relations for isotropic compressible elastic bodies. The method used may be extended immediately to isotropic incompressible elastic bodies. In that theory however, non-homogeneous deformations are allowed E5]. In consequence we may have universal relations holding only at a point in the body. Equations (11) remain unaltered but added to them is the incompressibility condition A~ ~2 ~3 = 1. REFERENCES [11 J. L. ERICKSEN, J. Math. Phys. 34, 126-128 (1955). [21 R. S. RIVLIN, Proc. 2nd Tech. Conf. (London, June 23-25, 1948) Cambridge: Heffer. [3] C. TRUESDELL, and W. NOLL, Handb. der Physik III/3, w (1965). [47 C. TRUESDELL, and R. TouPIN, Handb. der Physik III/1, w (1960). E5] J. L. ERICKSEN, Z. angew. Math. Phys. 5, 466-486 (1954). Zusammen/assung Es wird eine Methode zur Erhaltung allgemeingiiltiger Beziehungen ftir Verzerrungen kompressibler, isotroper, elastischer K6rper dargestellt. (Received: April 12, 1966.) The Swirling, Radial Free Jet in the Presence of a Transverse Magnetic Field By NORMAN RILEY, School of Mathematics and Physics, University of East Anglia, Norwich, Great Britain The work described in the present paper is an extension of previous work by RILEY ~1] 1) and MOREAU [2, 3 7. The swirling axi-symmetric radial jet flow of a conducting fluid in the presence of an axial magnetic field is discussed. 1. Introduction When a conducting fluid flows in the presence of a magnetic field the effect of the force, of electromagnetic origin, acting on the fluid is such as to inhibit the flow of fluid across the lines of force. MOREAU ~2, 3 7 has demonstrated this quite strikingly in his study of a 1) Numbers in braekets refer to References, page 642.

Transcript of The swirling, radial free jet in the presence of a transverse magnetic field

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Vol. 17, 1966 Kurze Mitteilungen - Brief Reports - Communications br~ves 639

Then,

0 = aij t i j = 2 6 (4 + ~2)-1/2 (tll _ t22 _ ~ t12)

+ 2 [ 2 + 1 2 (1 1 \1121-11~[t13 { 1 (1 1 \1/2'/231

1 ~ ( 1 + 1 1/2 -1/2 { 1 - - (1 1 } t23] ,

and since ,~, e, /, are completely a rb i t ra ry we obta in RIVLIN'S universal relat ion

t l l - - t2. 2 = ~t12, together with tla : t~3 = 0 .

5. C o n c l u d i n g R e m a r k s

We have dealt here with universal relat ions for isotropic compressible elastic bodies. The method used m a y be extended immedia te ly to isotropic incompressible elastic bodies. In tha t theory however, non-homogeneous deformations are allowed E5]. In consequence we m a y have universal relations holding only at a point in the body. Equa t ions (11) remain unal tered bu t added to them is the incompressibi l i ty condi t ion A~ ~2 ~3 = 1.

R E F E R E N C E S

[11 J. L. ERICKSEN, J. Math. Phys. 34, 126-128 (1955). [21 R. S. RIVLIN, Proc. 2nd Tech. Conf. (London, June 23-25, 1948) Cambridge: Heffer. [3] C. TRUESDELL, and W. NOLL, Handb . der Phys ik I I I /3 , w (1965). [47 C. TRUESDELL, and R. TouPIN, Handb . der Phys ik I I I /1 , w (1960). E5] J. L. ERICKSEN, Z. angew. Math. Phys. 5, 466-486 (1954).

Zusammen/assung

Es wird eine Methode zur Erha l tung allgemeingiil t iger Beziehungen ftir Verzerrungen kompressibler, isotroper, elastischer K6rper dargestellt.

(Received: April 12, 1966.)

T h e S w i r l i n g , R a d i a l Free J e t in t h e P r e s e n c e of a

T r a n s v e r s e M a g n e t i c F ie ld

By NORMAN RILEY, School of Mathematics and Physics, Univers i ty of Eas t Anglia, Norwich, Great Br i ta in

The work described in the present paper is an extension of previous work b y RILEY ~1] 1) and MOREAU [2, 3 7. The swirling axi -symmetr ic radial je t flow of a conduct ing fluid in the presence of an axial magnet ic field is discussed.

1. I n t r o d u c t i o n

When a conduct ing fluid flows in the presence of a magnet ic field the effect of the force, of electromagnetic origin, act ing on the fluid is such as to inh ib i t the flow of fluid across the lines of force. MOREAU ~2, 3 7 has demons t ra ted this quite s t r ikingly in his s tudy of a

1) Numbers in braekets refer to References, page 642.

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two-d imens iona l j e t in a t r a n s v e r s e field a t low m a g n e t i c Reyno lds n u m b e r . The so lu t ion ob ta ined , wh ich is qu i te ingenious, m a y deve lop a s ingu la r i ty a t a f in i te d i s t ance in wh ich case m o t i o n in t he or ig inal d i r ec t ion across t he l ines of force is a r re s t ed a n d t he f luid flows ou t a long t he d i rec t ion of the m a g n e t i c field. The presence, or otherwise , of th i s s ingu la r i ty depends u p o n t he d i s t r i b u t i o n of the field.

RILEY [1] showed t h a t a s imi la r i ty so lu t ion of t he a x i - s y m m e t r i c b o u n d a r y - l a y e r equa t i ons w i t h a swir l ing c o m p o n e n t of ve loc i ty m a y be o b t a i n e d in t he absence of a p ressure g rad ien t . This so lu t ion was used to discuss t he p roper t i e s of va r ious r ad ia l j e t - t y p e flows. I n t h e p re sen t no te i t is shown t h a t , despi te t he a d d i t i o n a l compl ica t ions in t he equa t ions , a s imi l a r i t y so lu t ion is sti l l ava i l ab le for rad ia l f ree- je t flow w i t h a swir l ing c o m p o n e n t of ve loc i ty w h e n t he f luid is c o n d u c t i n g and the re is a n axia l magne t i c field. I t is shown t h a t , d e p e n d i n g u p o n t h e r ad ia l d i s t r i b u t i o n of t he axia l field, a s ingu la r i ty m a y deve lop as in t he two-d imens iona l case. I n such cases m o t i o n across the l ines of force ceases, all t h e f luid f lowing ou t in the axia l d i rect ion. I t is also shown t h a t the p ro jec t ed s t r eaml ine p a t t e r n , up to th i s s ingular i ty , is una f fec ted b y t he field.

The t y p e of j e t flow env i saged here m a y be p roduced b y a f ini te disk r o t a t i n g in a t r a n s v e r s e field. The flow over t he d isk i tself has been considered, for example , b y I { A K U T A N I [4].

2. The S imi lar i ty Solution

The b o u n d a r y - l a y e r equa t i ons gove rn ing t he flow descr ibed in w 1 are

02u Ou Ou w ~ #2 a H ~ u + v - - u ~ + v Oy x e OY ~ '

(1) 0W 0W U W #2 O~ 02W

u O x + v Oy- + x e OY 2 '

0 ( z u ) + 0 ( x v ) = 0 (2) o~- o y �9

I n these equa t ions /~ t he pe rmeab i l i t y , a t he conduc t iv i ty , Q t he dens i ty a n d v t he k i n e m a t i c v i scos i ty of t he fluid, are all a s s um ed cons t an t . The coord ina tes x and y are in t he r ad ia l a n d axia l d i rec t ions respect ive ly . Axia l s y m m e t r y ha s been assumed. The ve loc i ty c o m p o n e n t s u, v are in the rad ia l a n d axia l d i rec t ions a n d w is t he swir l ing c o m p o n e n t of veloci ty . The m a g n e t i c field H 0 = H o ( x ) is in t he y -d i rec t ion a n d t he m a g n e t i c Reyno lds n u m b e r is t a k e n to be suf f ic ien t ly smal l to ensure t h a t t he field is u n d i s t o r t e d b y t he f luid mot ion . I t is a s s u m e d t h a t t h e r e is no e x t e r n a l l y appl ied electr ic field. I t can also be shown t h a t , w i t h i n t he f r a m e w o r k of b o u n d a r y - l a y e r theory , t he i nduced electr ic field m a k e s no c o n t r i b u t i o n to these equa t ions . W i t h s y m m e t r y a b o u t t he p l ane y = 0 t he requ i red b o u n d a r y cond i t ions for th i s f ree- je t flow are

Ou Ow v Oy Oy - - O , on y = 0; u , w - > 0 as y + oo. (3)

The c o n t i n u i t y E q u a t i o n (2) implies t he ex is tence of a s t r e a m func t ion ~o such t h a t

X ? A - - X V ~ - - Oy ' Ox "

Fol lowing RILEY [1] we seek a s imi la r i ty so lu t ion of E q u a t i o n s (1) a n d (2) in t he fo rm

W = ] / ; A x gl(x) I ( v ) , V = ~ x - l g2(x) y , w = A2 e x-~ g3(x) /'(V) . (4)

Here t he q u a n t i t i e s A and e are c o n s t a n t s and /(7) is t a k e n as

1 / = t a n h ~ ~/. (5)

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T o c o m p l e t e t h e s i m i l a r i t y s o l u t i o n t h e q u a n t i t i e s gl(x), g2(x), a n d ga(x) a re to b e d e t e r m i n e d s u b j e c t to t h e c o n d i t i o n t h a t for e = H o = O, gl = [1 + 13/x3J1/8 a n d g2 = [1 + I3/x3]-2/3. [n t h e s e e x p r e s s i o n s t h e c o n s t a n t l is a c h a r a c t e r i s t i c l e n g t h a s s o c i a t e d w i t h t h e j e t d e v e l o p m e n t .

I f we s u b s t i t u t e (4) i n t o E q u a t i o n s (1) we h a v e , w i t h a p r i m e d e n o t i n g d i f f e r e n t i a t i o n w i t h r e s p e c t to ~ a n d a d o t t h a t w i t h r e s p e c t to x,

74o2 : (6)

g, g, : x g , L g, g~ '

w h e r e ~ 0 ~ -- #s a / A = 0 H~. F o l l o w i n g t h e i deas i n t r o d u c e d b y 1V[OREAU [2j w e n o w w r i t e

X s (g, : g q = 1+ d g~(*)' .gs- + g~ : (71

g-~ \ x g ~ g ~ : g~ & J ' & - ga : '

a n d s u b s t i t u t i n g i n t o (6) t h o s e e q u a t i o n s m a y be r e d u c e d , b y v i r t u e of (5), t o

g s / / " + g , / ' S + g 4 1 ' = O , g s / / " + & / ' S + g 4 1 ' = O . (8)

C l ea r l y we r e q u i r e g5 = 7% g4, g6 = g7 = ks g4 a n d , u s i n g (5), t h e c o n s t a n t s k 1 a n d ks a re d e t e r m i n e d as k~ = 1, k~ = -- 2. T h u s , t h e e q u a t i o n s s a t i s f i e d b y t h e fou r q u a n t i t i e s gi(x) (i = 1 . . . 4) m a y b e w r i t t e n as

74~ : g~ -- g4, (9)

(fflg2 "~ ~X-<I I g 2 ] = 1 + g4 ' gsg~1-{ 1 + \ (-xegag' g2 ]I' "%" < ' * g : ' l = g s -) 1 - - 2 g , ,

g l (lO) g L ( 1 - x g a _ ] = 1 - - 2 g , . gs ga ]

U s i n g (9) t o e l i m i n a t e g4 in E q u a t i o n s (10) we f i n d t h a t s o l u t i o n s of (10), w h i c h g ive gl = [ 1 + la/x3] 1/3, & -- [1 + la/xn]-s/a w h e n e = H 0 = 0, a r e

g~ = x - ~ [ ( : - :)s/, + zs]~/s (1 - F?m, | g s = x ( x s - e s ) l / s [ ( x s - e s ) a / s + l s ] - s / s ( 1 - F ) ~ / = , ] (1i) g . = x [ ( : - : ) , i s + lnj-ws (1 - F ) .

w h e r e x

f ( x ) = / 2 ~ X (x 2 -- 82)-I/2 [(x 2 -- E2)3/2 q- /8]1/8 ~X" (12)

I n (12) t h e c o n s t a n t a, l ike l, is a s s o c i a t e d w i t h t h e d e v e l o p m e n t of t h e j e t a n d m u s t be c h o s e n so t h a t a > e if l 4= 0. W h e n e = 0 t h e r a d i a l a n a l o g u e of M o r e a u ' s s o l u t i o n is o b t a i n e d a n d w h e n H 0 = 0 R i l e y ' s s o l u t i o n is r e c o v e r e d .

T h e f o r m of E q u a t i o n s (11) a n d (12) i n d i c a t e s t h e p o s s i b i l i t y of a s i n g u l a r i t y o c c u r r i n g in t h e so lu t i on . As a n i l l u s t r a t i o n we t a k e t h e s i m p l e s t case p o s s i b l e in w h i c h a = l = 0 a n d t h e m a g n e t i c f ie ld is c o n s t a n t so t h a t ~ = c o n s t . F r o m (11) a n d (12) we t h e n h a v e

g2 = X (::2 e2)-i/2 (1 -- ~].~o ~ X2)I/~, g~ = x (:: - :)-,/~ (1 - 7402 :).

(131

ZAMP 17/41

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Clearly t he so lu t ion b r e a k s d o w n w h e n ~/0 ~ x = 1, m o t i o n across t he l ines of force is de s t royed a n d t he f luid is def lec ted in t he y -d i rec t ion para l le l to t he l ines of force. W h e t h e r or n o t b r e a k d o w n of th i s t y p e occurs depends u p o n t he r ad ia l d i s t r i b u t i o n of axia l field.

I t shou ld be n o t e d t h a t , as w i t h all s imi la r i ty solut ions, t he scope of so lu t ion (4) is l imi ted a n d i t m a y on ly be expec t ed to offer a desc r ip t ion of t h e flow a t rad ia l d i s t ances c o m p a r a b l e w i t h a d i s t ance w h i c h is n o t less t h a n t he m a x i m u m of l a n d a.

The e q u a t i o n of t he p ro j ec t i on of a s t r eaml ine on to t he p lane y = c o n s t a n t is unaf fec ted b y t h e presence of t h e m a g n e t i c field as long as m o t i o n across t he l ines of force persists . For , if t is t he angu l a r co-ord ina te , comple t i ng a s y s t e m of cyl indr ica l po la r co-ordinates , t h e n t h e p ro jec t ions in ques t ion h a v e e q u a t i o n s g iven b y

d l w e or

- - s i n ( 4 0 - 4 ) ,

where ;~0 is a c o n s t a n t . W e m a y note , f inal ly, t h a t w h e n a m a g n e t i c field is p resen t , t h e r e are no obv ious

i n t e r p r e t a t i o n s for t h e c o n s t a n t s A a n d e in t e r m s of t he f lux of m o m e n t u m a n d angu la r m o m e n t u m in t h e jet .

T h e a u t h o r is i n d e b t e d to Dr. H. K. MOFFATT for d r awing his a t t e n t i o n to the work of M. MOREAU.

R E F E R E N C E S

[1] N. RILEY, Quar t . J . Mech. App. Math . 15, 435 (1962). [2] R. MOREAU, Comptes R e n d u s 2 5 6 , 2294 (1963). [3] R. MOREAU, Comptes R e n d u s 2 5 6 , 4849 (1963). [4] T. KAKUTAI~I, J. Phys . Soc. J a p a n 17, 1496 (1962).

Z u s a m m e n ] a s s u n g

Diese A r b e i t i s t eine E r w e i t e r u n g f r t iherer A r b e i t e n yon RILEY [1] u n d MOREAU [2, 3]. Der wi rbe lnde a c h s e n s y m m e t r i s c h - r a d i a l e S t r a h l e iner l e i t enden Fl t iss igkei t in G e g e n w a r t e ines ax ia len m a g n e t i s c h e n Feldes wird u n t e r s u c h t .

(Received: April 19, 1966.)

R e m a r k s o n t h e B 6 n a r d a n d R e l a t e d S t a b i l i t y P r o b l e m s

B y R. L. SANI, Div. of Chemical Eng ineer ing , U n i v e r s i t y of I l l inois U r b a n a , Il l inois, U S A

I n i nves t i ga t i ng t he s t ab i l i t y of a th in , h o r i z o n t a l f luid layer h e a t e d f rom b e n e a t h t h fol lowing e q u a t i o n arises f rom t he m e t h o d of smal l d i s t u r b a n c e s for m a r g i n a l l y s t a b l s t a t i o n a r y d i s t u r b a n c e s (cf. [ I ] : ) , or [4])

M 3 w = ~ a ~ w . (1

Here M ---- - ( D ~ - - a2), D = d / d x , 4 is t he Ray le igh n u m b e r (a r ea l -va lued p a r a m e t e r a n d a > 0 is t he wave n u m b e r of t he d i s tu rbance . The b o u n d a r y cond i t ions a t x = 0 a n

1) Numbers in brackets refer to References, page 645.