QC 27 .mMA .#\43 MITLibraries Document Services Room 14-0551 77 Massachusetts Avenue Cambridge, MA 02139 Ph: 617.253.5668 Fax: 617.253.1690 Email: docs@mit.edu http://Iibraries.mit.edu/docs DISCLAIMER OF QUALITY Due to the condition of the original material, there are unavoidable flaws in this reproduction. We have made every effort possible to provide you with the best copy available. If you are dissatisfied with this product and find it unusable, please contact Document Services as soon as possible. Thank you. Some pages in the original document contain pictures, graphics, or text that is illegible. AME2H0D OF CORIMAZDII1G HE&T TRANSF) 30A BURFACE RAfINO. tUI by Warren m. Robsenovu A method based an a logical uxplanation of the meani of beat trans- fer associated with the boiling process is presented for correlating heat transfer data for nucleate boiling of liquids for the case of pool boiling. Tbe suggested relation is 1/As - I.7 iere the various fluid properties awe evaluated at the saturation tempera- Stre correspondinag to the local pressure and C5g is a function of the particu3w eatn sranfeat for cbatonetinfov witbout boiling is correrd Lated by the nomal baselt umaber, Rsynolds umber based on pipe diameter and Pwaudtl umber. For pool boiling with essentially saturated liquids, Jakob (1) rg; dasacusets nstt1 t o e ocx a tProessr shovs that the heat transfew from the surfae is for the most part transferred directly to the liquid, the increased heat transfew rate assaoiated with boillug being accounted for by the resulting agitation of the fluid by motian ofthe liquid flowlan behind the wak. of te bubble departing from the surface. Ilohsenov and Clark (2) showed a siinrlar result in studying notion piotteres e M~o~dama (3) for subco.le4 liguldsi heili but ?lowicg in luacised convection withi suface o uet gention of 'eaer-, Kurtther and greith (4) and Gunther(5) -2presented photographic evidence that in highly subcooled liquids in pool boiling and in forced ocnvection with surface boiling, the bubbles oould fona at the surfaoe pow, and then collapse ile remaining attached to the sur- eovertheless the increased heat transfer in boiling we attributed to face. The agitation of the liquid by the bubble notion. As the rate of heat transfer s increased and bubble agitation beemes more vigorous the effect of forced convoction fluid velocity and hence Reaolds maber based on pipe diameter becomes less and less. This effect is showm by the data of rohsenow and Clark (6) reproduosd here in figures 1 and 2. Wis data is representative of data of others for surface boiling with forced convection. In these figures the curves for various fluid velocities are seen to merge into one curve, showing that as the boiling becaes more vigorous, the effect of fluid vel<eity disappears. It seen reasccable then to seek.a correlation of the heat transfer data by meas of a bubble Reynolds umaber based on bubble diameter and velocity. For purposes of analysis one can visualse a number of streams of bubble receding from the heating surfaoe and a bubble Raynolds nmber defined by -tlhe mass velocity of the bubbles and their diameter as they leave 111 at 4 numbow *U-16 * Mis quantity is a measure of the local agitation of the fluid s0~g urfaee and hence is analogous to the ordinary pipe Reynolds s aeasure of the turbulence in the stream. To eam&$ate te bubble REynolds number, characteristics of bubbles in pool boiling will be employed since there is more detailed visual evidence available for this case than there is for forced convection surface boel . w 3 04 Results of these bubble characterics are ompi4ed by Jakob. (1). The heat transfer to the babbles while attached to the surface can be written with good appradaation (2) as (2) f Ir Frita (8) presents a relation for the diameter of the bubble as it leaves the surface, mhich may be written in the fom Fgi~~awhere - -o- -m(3) is the angle of centact of the bubble as sheen in figure 3. Jakob (9) has shoun for vapor bubbles of water and of carbon tetrachloride a relation sdts btmen te frequency of bubble formation at a favored point ca the smfae and the diter faco. of the bubble when it leaves the sur- Tis relation an be aprcated by the equation f~c UC Coge~mftn .. amma W ithout serious error. Inspecting the terms of equation (2) in the light of equations (3) and (4) @hows that (q/A)b is proportonal to a for a given operating pressure, it - sin* all other quantities are functions of saturation pressure alcm. or are oconstant. Experiments have shown that bubbles forM at selective points on surface forming swaying cols of bubbles. Jakob (7) found that the nmber of celvme or points of origin of bubbles mas very nearly directly proportional to the rate of heat transfer from the heating surface for a given operating pressure. Terefore q/A ~ (q/A)b and cn be written as where Cq may be a function of pressure. The mass velocity of the vapor bubbles leaving the surface may be written as - rquettions (3), -(6) - (5) and (6) may be substituted into equation (1) to obtain an expression for the bubble Reynolds number as - - - where Caw , Gb and n have been eliminated, and CR 5/y$--- is dimensionless and (7) The term . has the dimensions radians of angle. In applying this reasoning to attempt to correlate heat transfer data in the boiling regime it would seem that a bubble Nusselt number would be useful, defined as -I --W This quantity has been defined and utilised by Jakob (1)(16). - - (8) Substituting equation (3) into equation (8) results in - - - -J(9) A~- hre = ECd ere, too,, the term ///y * f.f) is. Sta:e the postalated aechanism of heat transfer indicates that most of' - 5 - the heat transfer goes directly from the wall to the liquid, and since the Prandtl umber is significant in relatiJufor heat transfer to a non-boiling fluid, it abould probably be included in the oorrelation for beat transfer to a boiling fluid. then the correlation suggested is Nxq w Np,(10) jP where -/iS1 t, are aln evaluated at the saturation tempers- C ture corresponding to the local pressure. The above relation applieS to the region of vigorous boiling ihere the fluid velocity or pipe Reynolds number does not influence the heat transfer rate. of pool boiling. It would also apply to the case In the case of surface boiling with forced convection and not very vigorous boiling bere the fluid velocity does influence the heat transfer rate, some form of a pipe Reynolds number might be added to the right side of equation (10). There is some doubt that the ordinary pipe Reynolds number would be significant because the notdon of the bubbles might tend to destroy the norml relationship between viscous and inertia forces. CtStat AnGE. The bubble contact angles values of C* T. n4 0; , shown in figure 3, is determined by the hence it is fluid and the kind ofheatng suface. detemined both by the kind of All of e other properties in the expressions- for bubble Reynolds muber and bubble Musselt numbers are fumctions of the fluid alone. he angle 9 from 'fire 3 iseen to be related to the various surface tensions by the relata Cos qv ioa........ w() -o - -o - For lack of available inforimation th" effec-t of pressure on $ was * - -- disregarded in applying equation (10) to existing data. This assumption is equivalent to assuming that the effect of pressure on the values of and of figure 3 is such that the angle a4 pressure. In applying equation (10) to the correlation of experimental data the terms CR' Cn and j Ef- L remains independent of will be omitted. Liauid SubgolUn In pool boiling the primary region of interest is the case in which the liquid temperature is essentially at the saturation temperature. However, In forced convection with surface boiling the liquid temperature may be greatly subcooled. It has been shown by many experimenters that the effect of sub- cooling of the liquid may be eliminated if the data is pintted as q/A vs T Hence defining the film coefficient in the as shown in figures 1 and 2. bubble Nusselt number ash 1 * ((/A)-i Tx eliminates the necessity of includ- ing liquid subooling as a variable in a correlation. OTHER FO3t F7THE P1DPOSED 00RE1L&TION LUATIMN Since both the bubble Reynolds number and the bubble Nusselt number embody a (q/A) term, it will be desirable to employ the tezu 'to Ce (12) This dimer sionless group is the ratio of liquid superheat enthalpy at the surface temperature to the latent enthalpy of evaporation. The equation (10) may be replaced by Pool Boiling: The proposed correlation equation (13) has been applied to the data of ni'ous experimenters. It vll hof in treat so observi in som deital) ik application to the data of Addes (10) for pool boiling of water because of the wide range of pressures covered -- 14.7 psia to 246 5 psia. In these experiments degasssed, distilled water was boiled by an electrically heated Data for a wire diameter of 0.024 inches is shown in horisontal platima wire. figure 4a. A plot of (q/A)/4 1g q0" 1 vs C (-, On this plot the position of the lines rises to a axi- isshown in figure 4b. am. with pressure and then falls again. At the pressure corresponding to the highest line on this plot, the Prandtl amber is very nearly at its minim value according to the data tabulated by Welum= Hence this effect (11). appears to be a Prandtl naber effect, which was anticipated in the analysis. A cross-plot of / , N,, for constant values of bubble Reynolds aumber shows the slope of the line on a log-log plot to be approximately 1.7; hence the final correlation as shown in figure 4c results in an equation of the form a~) ' C where the value of C 7 -- ----- - (14) is 0.013 with a spread of data of approximately - 20%. This process was repeated for some of the data of Cichelli and Bonailla (12) who boiled various fluids on a polished chroniu :.plated, hortsontal pleate which was electrically heated. shown in figures 5 through 7. form of equation (14). The results of the preposed correls tion e,e In each came the resulting equatione are (- tf Only the data for sing. component fluids on alcn surfaces were correlated, The data of Cryder and Finalborgo (15) i In every case the correlation equation (14) of C ,ire listed in. Table I. snown correlated in figure 8. ra6 applietd and the resulting- valuvet [Eai Flui an urface 28f Water - PlatiM a Addems(10) Ciabelli-Banilla(12) Bensene - 0.013 Crit 0.010 Cichelli-Bonilla(12) Ethyl Alchol - Chromite 0.0027 Cichelli-Bonilla(12) n-Pentane-Cromium 0.015 Cryder-Finalborgo(15) water - Brass 0.0060 &ArgAd Comeon~wt Buf Soilina: In order to show the effect of forced convection flow on the boiling process plots of vs (sifT) C t were u, made for the sur- ) face boiling data of Robsenow and Clark (6)(13) for degassed distilled water flowing in a vertical nickel tube 0.180' diameter 9.4N long and for the data of Kreith and Suimerfield (4) for degassed distilled water flowing in a stainless steel tube 0.587' diameter 17.5' long. Superimposed on these plots, figures 9 and 10, is the correlation line for the pooling boiling data for water from figure 4c. Lines of constant forced convetion velocity and pressure are seen to merge toward a single line whicb would probably be parallel to this line for pool boiling from figure 4a. When the boiling tecomes more vigorous at the bigher values of T, the effect of forcd eiuwction fluid velocity apparently disappears. In this region the motian o' th- bubbles seem to control th mechaniam of heat tasmfer due to fluid egitat.ion. In these correlations the fluid properties have been evaluated as properties of liquid at the saturation temperature. This was done both for the case of pool boiling with saturated liquid and for the case of surface boiling in forced convection of a subcooled liquid. Ir. each case the liquid near the heating surface is very nearly at saturation temperature or possib.; even at a nestastable superheated temperature. Properties of the liquid were used for tbe C./ , and k values in the bubble Nusselt number, the Pr' dti numbor, ad te new ters because the heat transfer wa found to occur imarily by transfer of heat directly from the heating surface to the liquid. The value of 4 of the bubble Reynolds mabhr was evaluated as a property of liquid because viscous forces acting to retard the notion of the bubble are those of the liquid. The results shown in figures 4 through 10 are essentially plots of q/A ' '' each muliplied by a judious oabination of fluid properties thus effecting the correlation. .mall changes in T. It is readily observed that q/A rises rapidly with FNrthes, the magnitude of Tz is rather mall, being of the order of 50 ? for water at atMospher 10 F for water at 2000 psia. pressure and of the order of 5 or Inallof the data oorrelated here the energy was suplied by electricityj hence T became the dependent variable in each case. It is difficult to measure the heating surface temperature directly when electric heating is employed. It must be calculated from other measured values such as outer tube surface temperature or resistance of the heating wire. The value of TZ is obtained by subtracting the saturation temperature from this determined heating surface temperature. Since the agnitude of T. is s=m1 any errors in the determined value of heating surface temperature will be greaz magnified in the resulting value of Ty. This can. possibly account for some or' the cifference in the value of C of equation (14) as obtained by variou experienters. It ia, of course, evssntial in obteining a correlation of data that the p f the fjald employ-ed be n;recZ. a error :n the vaues i : - 10 - properties is directly reflected in the data correlation. Probably the most significant cause of the difference in the values of C is the result of emittiag, for lack of currently available information, the ters frm the bubble Reynolds number and the, bubble Nusselt number in arriving at the oorrelation as applied. be a fwnotian of P *ih The effect of this is to cause C to is deterained by the character of and the kind of heating surface and by the properties of the fluid as shown by equation (11). There is then good reason to expect a different value of C to result for every cimnation of kind of surface and kind of fluid. Additional infomtion regard- ing the values of f for various combinations of surfaces and fluids should clarify this matter and produce a valid correlation for all such combinations. In arriving at tquation (5) and hence equations (7) and (9), the expressions for bubble Reynolds nmber and bubble lusselt number, it was assumed that did not vary with pressure for a particular ombination of fluid and heating surface. This assption y account for same of the small spread of the final correlation for each surface.-fluid combination. The assumption appears to be fairly good, nevertheless, since Vie data for a particular fnwidheating surface ocabination is correlated within about t 20% by equation (14).a It is not suggested that the exponents 0.33 and 1.7 of equation (14) are the tme values nor that the form of equation (14) is the best one. Rather i in suggested that the dimensionless groups -if equation (14) are significant in correlation boiling heat transfer data, presented here. Much more data was correlated than 14n Only the data for single omponent fluids on clean surface* are presented here. They semed to be correlated quite adequately by equation, (14) with the exponents of 0.33 and 1.7. The 0.33 expopent of the bubble Reynolds number appeared to be adequate for most of the data whether the heat,ing surface was clean or not, but the 1.7 exponent appearel to be valid on.ly for clean surfaces. With dirty surfaces the vAlue of thia exponent wat at -. -~ - - - - - - - - - ___ 11 - erratic, varying between 0.8 and 2.0. For purposes of comparison the oorrelation equation (4) may be re-written in the form a=IA IVA- N NR, nayhbe owtpared C41 - (15) Npe the non-boiling fomed ocavection exression C, NkRe NN . .. , qwere tht is in the range of 0.5 to 0.7 men the flow area varies along the direction of flw, e.g., for flow across tubes, around spheres or cylinders, or across interrupted tins. Data for pool boiling of a liquid on a clean surface an be correlated by an equation of the forms CCAA Further eaperimental work is needed to study the variation of bubble contact angle and coefficient C with pressure ad with type of heating su- face fluid combination. Further experimental work is needed to study the validity of equations (3), (4) and (5) uhich were used in obtainin tbe terma bubble Reynolds number and bable Nuaetlt vumtr. j T; - 12- Ths3ka are due to Dr. J. N. Addmcs for permia=w"u to us his data shoun in figure 4 and to Mr. Fakhri Rahmatasah for perfoming most of the calcuiations required in preparing this report. - Cd,Cfd, Cq, 13 - Coefficients in equatians (3),(4),(5),(9),(7), respectively. Cnf CR C Coefficient of equation (14), a&ih depends upon the nature of the heating surfacefluid ccibination. Db Dameter of the bubble as it leaves the heating surface, ft. Mass velocity of bubbles at their departure from the heating e@, Nush 4 ftp. Bubble Rusiselt niuber, defined by equations (8) and (9). NPR 0 NRe,b T Bubble Reiynoads nmber, defined by equations (1) and (7). Heag surface temperature minus saturation temperature, F. Specific heat of saturated liquid, Btu/lb *O f Frequency of bubble foimation, lAr. g Acceleration of gravity. Ccnversion factor, 4.17 a 10 f (lb mas)(ft)/(hr)(potwso force.) Latent heat of evaporation, Btu/lba q/A + !,, flm coefficient of heat transfer, BtA/hr ftayo Thermal oceductivity of saturated liquid, Stu/hr ft F. Nuaber of points of origin of bubble columns per fta of heating surface. (VA)b Beat transfer rate to bubble per unit heating surface area wAhol bubble remains attacbed to the surface, Btu/hr fte q/A Beat transfer rate per unit heating surface area, BtuAr ft 3 . Bubble contact angle, defined in figure 3. Qh ry'4 VnV. Surface tension of liquid-vapor interface, lb/ft Surface tension of vapor-solid interface, lbf/ft Surface tension of solid-liquid interface, lb./ft Density of aaturated liquid Iba/ft3 Density of saturated vapor lb./ft$ Viscosity of saturated liquid, lblft hr. 1. Jakob, M., 'Heat Transfer,' Vol. I, Chap. 29, Wiley, 1949. 2. Rohsenow, W. M. and Clark, J. A., "A Study of the Hochanim of Boiling Heat Transfer," ASME Trans., July, 1951. 3. Kennel, Minden, Rudoff, Picornell, Dew, 'Heat Transfer at High Rates to Water with Surface Boiling,' Ind. Eg. Chem. MeAdans, W. H. Vol. 37, No. 10, Oct., 1945, pp 1010-1016 4. Gunther, F. C. and Lreith, F., 'Photographia Study of Bubble Formation in Heat Transfer to Subooled Water," Beat Transfer and Fluid Mech. Inst. 1949, Berkeley, California, p. 113. 5. Gunther, F. C., "Pbotograho Study of Surface-Boiling Heat Transfer to Water with Fored Convection," AM Trans., Vol. 73, No. 2, Feb., 1951, p. 115. 6. Robsenow, W. N., and Clark, J. A., 'Heat Transfer and Pressure Drop Data for High Heat Flux Densities to Water at High Sub-Critical Pressures,' Heat Transfer and Fluid Medh. Inst., 1951, Stanford, California. 7. Jakob, M., 'Local Temperature Differences Occurring in Evaporation, Condensation, and Cats~ytto Reaction,' Temperature, its Measurement and Control in Scienc and Industry, Reinhold, New York, 1941, p. 834. 8. Frity, W., Physik. Zeitshr., Vol. 36, 1935, p. 37'. 9, Jakob, M., Zeitabr. d. Ver. deutsch. Ing. Vol. 76, 1932, p. 1161. 10. Addmma, J. N., "eat Transfer at Nig Rates to Water Boiling Outside Cylinders,' D.Sc. hesis, Chen. kgrg. Dept., Mass. Inst. of Tech., Jum, 1948. 11. Vel2aan, E. J., "Survey of Thermodync and Physical Properties of Water,' .8. Thesis, Jan., 1950, Purdue University, Lafayette, Indiana. 12. Ciaelli, M. T. and Boni1a, C. Y., 'Heat Transfer to Liquids Boiling under Pressure,' Trans. As. Inst. Chm. Engre., Vol 41, 755-787, 1945. 13. Clark, J. A., Malherbe, P., Mullin, F., and Robsenow, W. M., 'Heat Transfer Data for Low Velocity Forced Convection Flow of Water with Surface Boiling,' Tech. Rpt. #4, DIC Project 6627, M.I.T., July 1, 1951. 4. Kreith, F, and Sumierfield, M. J., 'Heat Transfer to Water at High Flux Densities,' Trans. ASME, Vol. 71, No. 7, Oct., 1949. 15. Cryder, D. 8., and Finalborgo, A. C., 'Heat Transmission From Metal Suf aces to Boiling Liquids: Effect of Temperature of the Liquid an Fila Coefficient,' As. Inst. Chem. Engrs. Vol. 33, 1937, p. 346. 16. Jakob, N., Proc. 5th Internat. Coqgr. Appl. echo., 1938, p. 561. Figure No* 1 Title Effect of Fluid Velocity an Heat Trafer Pat, in Nucleate Boiling (Data of Rohsenov and Clark,( ). Effect of Fluid Velocity oa Heat Transfer Rate In Nucleate Boiling. Data of Rohseuoo and Clark (6). Surface TeAsion forces Acting at Point of Bubble Contact. Correlation of hata of Addm (10) for latinum-Vater Interfaos for Pool Boiling. Correlation of Data of Ciel-Bsilla (12) for ChromiumBansene Interfacebr Pool Boiling. Cornlation of Data of Cihelli-Bnilla (12) for ChrominuMthl Alohol Interface for Pool Boiling. Correlation of Data of Ciohelli-Bcnilla (12) for Chraiu.n-pmntne Interfaee for Pool Boiling. Correlation of Data of Cryderinalborgo (15) for Brass-Water Interface for Pool Boiling. Data of Robsenow-Clark (6) (13) for Nickel-Water Interface for Forced Convetion Surface Boiling. Data of Kreith-4tmerfield (14) for Stainless Steel-Water interface for Forced Convection Surface Boiling. 5.0 4.0 3.0 2.0 1.0 0 x 0.5 cr 0.4 0.3 g 0.21- 60 100 200 WALL TEMP. - LIQUID TEMP. (*F) FIGURE I 4.0 IO 3.0 A A P =2000 PSIA Vi= 30 FT /SEC G I 0 A 5.7 x 106 LB / HR FT 2 2.0 -- 0 O0 20 FT/ HVi= c A. -- GG5.7xI p 2000 x 1.5 -p = 2000 PSIA PSIA 6 p=2000 PSIA LB/HR FT 2 p =150 PSIA Vi= 0 FT / SE Vj= 0 FT SECVi2O FT/ SEC G = .2 106 2 = .96x 10 LBHR T?-G =4.2x 10 6 LB/HR FT 2 LBFT2 FTI G9OLB/HR 1.0 3 Tx 89 7 4 5 6 = 5.7 106 L 10 20 15 R FIGURE 2 LIQUID VAPOR a'tv o'v s HEATING SURFACE FIGURE 107 100 100 xx A ox A 14.7 383 PSIA P S IA e 770 PSIA A 1205 1602 2465 PSIA 0 10 10 x 0 0 b PSIA PSIA A b 0 x. 0' Nn 0 A 1.0 0 gf x =0.0 x /A =0 y3 h fg g0 c g(Pe-Pv) 0- 33 (c / kt 0./ 0/ 0.1 104 0.01 C ADDOMS (10) POOL BOILING PLATINUM WIRE-WATER 0.024" DI AM. I 1111111 0.1 T hfg T hfg Npr'' FIGURE p 4 +^- 1O + o 465 + 645 0oD 0 b 00 x .0 0 0'0 x CICHELLI-BONILLA (12) POOL BOILING BENZENE ON POLISHED PLATED CHROMIUM x 1.0 3 C Tx g 0 0o. q/A h fg At h fg .3 c. g (p -pv) 0.1 0.01 hf TX N p' FI GUR E 10 - + A L / -it3A Z o 11 5 + 265 5 15 765 b0) CICHELLI - BONILLA (12 POOL BOILING ETHYL ALCOHOL ON POLISHED PLATED CHRC 1.00:> q/A a0 hg Tx =0.0027 .001 hg 90~ g(P-P ) 0-33C / 0.01 111 Tx 1.0 N 1pr' FIGURE 6 22 PSIA o A60 o + 10 A * 115 2 15 3 1 5 4 15 'I CICHELL I -BON ILLA (12) BOILI NG n- PENTANE ON POLISHED PLATED CHROMI POOL cT 1.0- £LTx = hfgg goa,- q/A . h fg gT(pt -pv ) 033 cIp )I.7 k.1 0.1 0.01 hfg X Npr'' 7 FIGURE 7 I I I 0.10 * 0 I 11111 I o 22.4 PSIA A 14.1 03 8.76 e o 4.31 2.05 b Q_ 0. CRYDER-FINALBORGO (15) 0' 1. 2 Ct 0.011 .0 01 POOL BOILING BRASS TUBE-WATER T. =0.0060 I I I I hfg (q/A hf ILL I I op;p)) g gpi~p-v) O.33 cl gA. kg II Iliii I I I ,01 pr FIGURE 8 CORRELATION LINE FOF ADDOMS DATA, FIG.4 ~5O V 100 '>' ob0 b 2000 PSI V=30 20 10 T-0 1.4 / / (b V 0.8 0.5 0.2 A 0.1 * 0.05 1500 PSIA + V=30 20 0 10 1000 PSIA v V =30 10 / / 0? 0 / ROHSENOW - CLARK (6)(13) FORCED CONVECTION SURFACE BOILING NICKEL - WATER 1.0 0.1 0.01 I h fg N '. FIGURE 9 100 I CORRELATION _ ADDOMS I /I I I LINE FOR DATA, / FIG. 4 p=157-168 PSIA o V = 6-7 FT/SEC a 12 100-110 o 6-7 12 60- 66 v 6-7 * 12 45.5 v 6-7 40.5 10 U 36 0 36 * ( 6-7 6-7 22.5-25 6-7 A '4- / / / 12 0 KREITH -SUMMERFIELD (14) FORCED CONVECTION SURFACE BOILING STAINLESS STEEL-WATER I I I I I I I 0.1 I 0.01 I hfg N 'r7 FIGURE 10 DISTRIBUTION LIST Chief of Naval Reseerch Department of the Navy Washington 25, D. C. Atta Code 438 (2) Director, Naval Research Laboratory Washington 25, D. C.. Attn: Tech. Info. Officer (9) Technical Library 11) 2) Mechanics Division Cammanding Officer Office of maal Research Branch Offtice 495 Sumer Straeet Boston 10, 4Mss. Cowwanding Offioer (2) (1) commands"g Oftswp sIearch Branch 01ft~g a44 N.V ah Chicage 2 1 Office of Branch 801 Doanafto Ban Frasnstag ! Office Branch t (1) #Miearch (1) Waif. Nserch 1030 0290IA Pasdn, Contrast A Offife 4C 1 (1) Area Departait Attas ibt , (2) Research and Development Board DepartAent of Defense Pentagon Building Washington 25, D. C. Attn: Library (Code 3D-1075) Chief of Bureau of Aeronautics Navy Department Washington 25, D. C. Atta: TD-41, Technical Library PP-22 Chief of Bureau of Or&ance Navy Department Washington 25, D. C. ' Office of gesel Research Branch Offt-Ig 346BrO4S New Yogg SO N Office argg1 Library of Congress Washington 25, D. C. Attn: Navy Research Section (1) Assistant hwftl Attache for Research London U. 3. -Mvy 00 OU SewYcrk, N.i. (.5; I Attat Ad-3, Technical Library (2) Chief of Bureau of Ships Navy Department Washington 25, D. C. Attn: Director of Research Code 390 Code 646 Code 432 (2) (3.) (2) (1) Superintendent U. S. Naval Academy Post Oraduate School Annapolis, Maryland (1) Naval Ordnance Laboratory White Oak, Maryland RFD 1, Silver Spring, Maryland Attnas Mechanics Division (1) Naval Ordnance Test Station Inyokera, California Atta: Scientific Officer (1) Director, Naval Engineering Experiment Station Annapolis, Maryland (2) Chief of Staff Department of the Army The Pentagon Washington 25, D. C. Attu 4 Director of Resparch and Pvelpmnt 4 U - -- W -- Distribution 14&-t',4j Office of Chief of Ordnance Research and Development Service Department of the Army The Pentagon Washington 25, D. C. Attn: ORDTB (1) Cemnanding General U. S. Air Forces The Pentagon Washington 25, D. C. Attns Research & Development Div. (1) Professor W. H. McAdams Department of Chemical Engineering assachusetts Institute of Technology Cambridge 39, Massachusetts, Office of Air Research Wright-Patterson Air Force Base Dayton, Ohio Atta: Chief, Applied Mechanics Group (1) U. S. Atomic Energy Comission Division of Research Washington, D. C. Argonne National Laboratory P. 0. Box 5207 Chicago 80, Illinois Attn W. H. Jens (1) (25) U. S. Coast Guard 1300 Z Street, N. W. Washington, D. C. Attn: Chief, Testing and Development Division (1) National Advisory Committee for Aeronautics Professor A. L. London Department of Mechanical Engineering Stanford University Stanford, California 71 (1) Professor Warren Rohsenow Mechanical Engineering Department Massachusetts Institute of Technology Cambridge 39, Massachusetts (15) Lt. Cdr. E. P. Wilkinson c/o U. 8. Atomic Energy Commission P. 0. Box 1105 Pittsburgh 30, Pa. (2) Mr. R. A. Bowman Westinghouse Electric Co. Atomic Power Division P. 0. Box 1468 Pittsburgh, Pa. (1) Dean L. M. K. Boelter Dept. of Engineering University of California Los Angeles, California (1) Professor J. H. Keenan Dept. of Mechanical Engr. Mass. Inst. of Technology Cambridge 39, Massachusetts (1) Professor J. N. Addoms Dept. of Chemical Engr. Mass. Inst. of Technology Cambridge 39, Mass. (1) Dean W. J. Woblenberg School of Engineering Tale University New Haven, Conn. (1) Cleveland Municipal Airport Cleveland, Ohio Attas J. H. Collins, Jr. (2) Dr. William Sibbitt Purdue Research Foundation Purdue University Lafayette, Indiana (1) Professor E. D. Kane University of California Berkeley, California (1) Dr. J. V. Foa Cornell Aeronautical Laboratory Buffalo, New York (1) Professor John W. Hasen Engineering Research Division University of California Los Angeles 24,4 California (i) Mr. E. E. Ross Room 20-E-226 Mass. Inst. of Technology Cambridge 39, Mass. Distribution Also to Include the Following Mr. Gilbert I.. Capbell Library Los Alamos Boientific Laboratory P. 0. Bo= 1663 Los Alamos, New Mexico (3) Comiande e BRoth Office of Chicago Directed Operations U. 8. Atomic Bnerg Commission P.O . Bo 46 A Chicago 60, lnois (1) J. C. Morris Chief Librarian Oak Ride National Laboratory P. 0. Box P Oak Ridge, Tennessee (3) r. a. Etherington, Director Naval Reactor Division Argonne Natonal Laboratory P. 0. Box 5207 Chicago 80, Illinois Miss Rasel futoheson, Librarian Westinhoue Electric Corporation Atomio Power Divisi&n P. 0. Box 1468 Pittsbrgh 30, Pennylvania (3) Mr. Joel V. Levy Bureau of Ships Department of the Navy Washington 25, D. C. (1) Mr. Spencer C. Stanford Library Brookhaven National Laboratory Upton, Long Island, New !ork (3) Mr.W. e. houpp Director of Research Westingouse Eletric Corporation Atomic Power Division P. 0. Box 1468 PittsbOrgh 30, Penawlvania, (1) Library Pairhild Engine & Airplane Corp. NEPA Division P. 01 Box 415 Oak Ridge, Tennessee (3) Mr. Robert Bromberg Engineering Research Department of Engineering University of California, Los Angeles 24, California (1) (4) Mr. Den Pinkel National Advisory Committee for Aeronautics Lewis Flight Propulsion Laboratory Municipal Airport (2) Cleveland, Ohio Reference Services Branob Technical Information Servics U. 8. Atomic Bnerg Com4aon Oak Ridge, Tennessee Attns I. A. Warhit, Chief (4) Mr. E. P. Eransfelder Babcook & Wiloom Compay Research & Development Dept. Al liance, Chio Dr. George A. Hakins Purdne University Lafayette, Indiana (2) (1) #r. Fred Gunther Jet Propulsion Laboratory California Institute of Teohnolo (1) Pasadena, California Dr. R. U. INon Technical Division Oak Ridge National Laboratory Oak Ridge, Tennessee Mr. R. 8. Isbin Hanford Works P. 0. Box 550 Riahland, Washington (1) Mr. W. K. Woods (1) 3703 Building General lectric Compa Rchiland, Washington (1) Distribution (cont.) Mr. N. F. Lansing Oak Ridge National Laboratory P. 0. Bom P Oak Ridge, Tennessee (1) Mr. Frederick T. Hobbs Technical Cooperation Branch Division of Research ABC ashington, D. . (1) Mr. H. V. Lichtenberger Argonne National Laboratory P. 0. Box 5207 Chicago 80, Illinois (1) g. D. Young Information Division Argonne National Laboratory P. 0. Box 5207 Chicago 80, Illinois (2) d * John R. Hufftan Reactor hngineering Division Argonne National LaboratOry P. O. Bo: 5207 Chicago 80, I11Ani (1) Hr. Frank Kreith Project Squid Princeton University Princeton, New Jersey (1) Dr. Martin Serfield Project Squid Princeton University Princeton, New Jersey (1) Dr. Alfred 0. Lundquist Code 429 Power Branch Room 2714, Bldg. T--4 Office of Naval Research Department of the Navy Washington 25, D. C. (1) Mr. 0. . Woodruff, Jr. Physics Department Atomic Power Division Westinghouse Electric Corp. P. 0. Eox 1468 Pittsburgh 30, Pennsylvania (1)