Discover OCR-ed Pages Content

Displaying results 5126 - 5150 of 58712

Recirculatory flow in a cylindrical cavity

Sequence 36
-- 29 Therefore, in order for ) < 'll/ell , we must have,).. -E:. I and, since in our case ~ = 1, the solution is…
Sequence 37
30 APPENDIX II The integral e := j;k erf(/if :) [ <=xp l-'/~"i ~-J)~ _ e:.xp(-'/4-X)('f'f-J)…
Sequence 38
31 we have 19 This expression when integrated and simplified yields E = 2/~()( ... f)' frexp (- (r--Yj/f(X+<fJ…
Sequence 39
32 APPENDIX III The condition /1 AB 1/ tC 1/ A II /I B 1/ for the kernels given in equation 1-1 may be shown in the…
Sequence 40
33 or where H(r,jf ) is defined as the inner integral, and Z H 6 /tIRX'RJ (See Reference 20, p. 156) Thus (b 60 /…
Sequence 41
Now since we have :J l (e-) 0 27;;., { exp {-Ct. -~)X ,(~) -aP (-( to -t ctJ; x,j ] 4d z-) ~ l~ { cxPl- (Jo-?;)/1xJ - e!(P( -…
Sequence 42
35 REFERENCES 1. Prandtl, L., "Uber Flussigkei tsbewegung bei sehr kleiner Reibung," Proe. III International Math…
Sequence 43
36 17. Howarth, L., "On the Solution of the Laminar Boundary Layer Equations," Proc. Roy. Soc., London, A, 164, p.…
Sequence 44
1.0 .75 K .50 .25 FIXED FREE STREAMLINE STREAMLINE _{ERNST (th.l I ROSHKO (exp.) WOOD (th.) 0 SQUIRE (th.) • MILLS…
Sequence 45
ttl - Lf"l p:: :>. -.~ :>. 5.0-- 4.0 .. _ 3.0L. 2.0 , 1.0 + x/c a x/c '"It x/c v x/c…
Sequence 46
• C'j - 111 p::: >. /I ~ >. 4.0 + x/a 0 x/a lX x/a f7 x/a = 3.0 2.0 . 1.0 0.1 0.25 0.5 1.0…
Sequence 47
- til - II) p:: >. II ~ >. i 8. O~ 6. O~_ 4.0 2.0 I \ + x/c 0.1 0 x/c 0.25 ~ x/c 0.5 V x/c 1.0…
Sequence 48
- 10.<r I I I I I I I I 8.0- I I I I I I I I I i 6.0_ 4.0- 0.0 of- x/a = 0.1 a x/a = 0.25 J:t x/a…

Recirculatory flow in peripheral-jet supports

Sequence 1
PROJECT TUBER/DNT
Sequence 2
TR PT 6805 RECIRCULATORY FLOW IN PERIPHERAL-JET SUPPORTS by Chen-C. Sun This research was supported by the National…
Sequence 3
ACKNOWLEDGMENT The author wishes to express his appreciation and gratitude to Dr. Thomas J. Black for his guidance and con~…
Sequence 4
LIST OF SYMBOLS b H J k pa pc po R * r t = = = = = = = = = constant R - Po. if v:1. Pc. - Pc1. p .. -…
Sequence 5
INTRODUCTION One type of ground effect machine is designed so that the pressure of the air cushion is contained by a…
Sequence 6
- 2 - A major object of the present study is therefore to derive a more de- tailed analysis of the mixing process in a highly…
Sequence 7
- 3 - where VQ , V(" , f and t are tangential velocity component, radial velocity component, fluid density and the eddy…
Sequence 8
- 4 - We obtain (14) (15) so that 'dVe* 1/ e3h -4 J'(7) "0 r* = (16) d:J. V~f. -R 3 4,.b - 6 f'll…
Sequence 9
- 5 - 2. Preliminary Approximation Solution of Jet Mixing Process As discussed later in Section 4 a major objective of the…
Sequence 10
- 6 - In the case of the wall jet, the maximum velocity (which occurs at y = Y1) decreases steadily with distance along the…
Sequence 11
I Multiplying (25) by f (~) we get - 7 - Again integrate (26) from 7 to ~ yields Evaluating equation (27) at 7 ~ 0 results…
Sequence 12
- 8 - boundary conditions ~(o) = 0 ) if 1/( 00) .:;::. 0 (36) Equation (35) with boundary conditions (36) has been solved…
Back to top