chemical physics of discharges - Argonne National Laboratory

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Discussion and Results 560 Three briquettes of aluminum, lead and silver were made to test the validity of the experimental technique since their thermal properties were available from the literature as shown in Table I. Sintered, dense hematite (Fe 0 ) and a briquette of porous carbon 2.3 I made from a partially devolatized coal were used as test materials For these materials, all properties except the thermal Conductivities shown in Table I were previously measured. Cooling curves for each briquette were measured for a nitrogen flow rate of 0.9 scfm. Sur- face heat transfer coefficients for lead, silver and alumixC - vere calculated by the method discussed in the data processing section. For these materials , the llterature conductivity values were used to calculate the surface coefficient. Table I shows that the calculated or experiment@ h values for each metal are nearly identical. This result is consistent with the theoretical basis of the experiment and may be considered as establishing the validity of the method. Also as additional evidence, aluminum was choosen as the standard and k values for lead and silver were calculated using the h value for aluminum. Table I shows that the calculated or experimental k values were within 0.5 percent of the literature values. The conductivities for hematite and porous carbon were calculated using aluminum as the standard. Figure 3 shows the experimental data points with the solid lines , calculated from the theory. Note that the line for the carbon is curved whereas those for the metals and hematite are linear. As discuss- ' ed previously, a linear cooling curve is obtained if the surface to solid thermal resistance ratios are relatively large. Note that for the metals, lead which has the lowest conductivity and thermal diffusivity cooled the fastest. This result is explained by examination of eqn. (25) which shows that for similar gas flows and briquette dimensions, the rate of cooling for different materials is determined by the heat content, pC . It can be seen in Table I that the heat content for lead is the lowegt of all metals tested. . Summary A rapid, simple method for determining thermal conductivity for a solid has been developed. The solid can be either porous or non-porous and of either high or low conductivity. If high conductivity materials are tested, then both conductivity and heat capacity can be simultaneously measured from one cooling experiment. The method was validated by using the known thermal properties of lead, aluminum, and silver and the experimental cooling curves in a comparsion with the computed results. References 1- Newman, A. B., Industrial and Engineering Chemistry, Vol. 28, 1936, i pp. 545-548 . . _. .-. - . . . . . ., . . I 1 i 1 I 1 1
1 I A An ''P 'H I 'h I k ma "r Q R r ' S t /X tC tS xo I xr ! yx yr ( a I 1 8 I ! J \ *I e - 551 Nomenclature Half height of briquette; ft Area; ft2 Coefficient in infinite series solution for temperature dis cri- bution in Briquette Specific heat; BTU/lb OF Overall heat transfer coefficient; BTU/hr ft2 OF Surface heat transfer coefficient; BTU/hr ft2 .OF Thermal conductivity; BTU/hr ft2 O F / f t Axial surface resistance; dimensionless Radial surface resistance; dimensionless Heat flux; BTU/hr Maximum radius of briquette; ft Radius of briquette; ft Half width of infinite plate; ft Temperature; OF Temperature at center of briquette; OF Initial temperature of briquette; OF Temperature of cooling gas; OF Distance of direction; ft - - a8 Dimensionless time parameter for axial component 02 = a8 Dimensionless time parameter for radial component r2 = Symbol for temperature ratio, axial component; dimensionless = Symbol for temperature ratio, radial component; dimensionless =(k/eCp) Thermal diffusivity; ft2/hr = Time; minutes or hours = Density; wft3
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)i 1 reesonably complete and accura
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3 inquire about the component of ve
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4 I I 5 To find (t2)av, we assume t
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\ vnich, it is noted can be negativ
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I 7 than or smaller than the second
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i I i I I I ) ) i L , I I . INT1:OD
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13 field per electron is and per co
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. 11. 5. CharRe-Transfer and Ion-Mo
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17 In the followin:: sections much
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above. With that EIN, an estimate o
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21 region in w!iich large, nighlv l
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i ’ understanding: 23 (a) Electro
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Obviously, the secondary ion must h
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27 (22) Franklin, J. L., Munson, M.
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Tables 1-6 present examples of rela
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Table 8 Some Ions Formed by Process
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33 velocity of the reacting partn r
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35 must be added to the Langevin cr
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37 In our laboratory a microwave di
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+ . 4 . r 39 as well as N in a cor0
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ION-MOIECULE REACTION RATES MEASUFI
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43 excitntion 2onditions so that th
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45 In 2 like manner Fig. 3, showing
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47 Absorption Spectra of Transient
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50 maximum fiela. In this manner, a
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52 3 % %- %- 5- a- 7 h W P H 0 L v)
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References I I . A.B.Callear, J.A.G
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._ . _-.. - , , . . ,. . The Pyrex
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58 0 0 0 VI J > I cv . u H a
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.... . 0 2 e I / m 0 H F4 : 1
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\ 0.9 0.8 0.7 06 0.5 0.4 0.3 0.2 01
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65 ' cause of the reduction in the
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INTRODUCTION I' Attachment of polar
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I 69 EXPERIMENTAL The mass spectrom
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+ Figure 1 Mixed water and methanol
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73 ' , radius might be expected bec
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75 Negative Ion Mass Spectra of Som
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A b 1 1 I H I I I FILAMEN T CONTINU
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79 for positive and negative ions,
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51 out to answer some of the questi
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93 INTERACTIONS OF EXCITED SPECIES
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L 4 I*C z 0'2 = a, a U x I m 4 m 0
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I L I, ; > > E Fig. 3 I50 200 150 1
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I 300 r 1 - 200 i io ;' a cn I I. 0
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where DISCUSSION OF XESULTS PERTAIN
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93 where the bar indicates values c
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'I i 'I 0 2. 4 6 8 2 [ N]* x' I 0-2
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Fig. 14 IO 8 6 4F [NO] x IO-" (mole
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for chemiluminescent excitation in
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101 Chemiluminescent Reactions of E
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103 All gases were taken directly f
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10; He: + N2 -. 2He + h': (8) whi!?
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description for both diffusion and
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B. Ions and Electrons I Consider a
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' 112 axial diffusion through the d
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the tube walls occurs continuously
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E2R M ' $6"
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1. 2. 3. 4. 5. 6. 7. 8. 9- 10. u. -
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120 . Dlschorge zone Reactor zone 1
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122 In radiation chemistry the cust
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124 4. chemistry seem limited essen
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126 Conversion of Mixtures into Mor
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Hydrazine Synthesis in A Silent dle
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{;I . - . .. . - .., . . .. _- .. .
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1 \ \ \ , \ , \ \ Pmer hnrity K.W.
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. I operating fact that the sloGe i
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_- of ' . 8. - 7 6, Residence Time
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135 Ionic Reactions in Corona Disch
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GAS OUT GAS IN i.ho QUADRUPOLE MASS
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- + ( ~ ~ + 0 H ) ~ O ~ ( H~o)~H+ +
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144 i I , , , , . + 1- u 3c w Inu c
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146 SYNTHESIS OF ORGANIC COIGhTDS B
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mi5 a- dz CI n I a I n +4 - 0 -I- k
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0 z cu I I I
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I- I - t d m a .rl Y x c, t-' d k
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, 155 This result is significant in
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Compound Bond he rgy Li I 82 UBr 10
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, ”..’ 3or 25 - 5 20 - s 3 w Y
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I 161 THE GLOW DISCHARGE DEPOSITION
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Fig. 1 Process Apparatus -__l.ll__
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v) t- at- InIo Io0 t-Q) loo lcua O
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This study is only an approximation
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Mole Reaction Material ratio time e
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\ i (4) Effect of System Pressure T
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173 Pressure. Since pressure is a c
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175 Table VI X-RAY DATA OF DEPOSIT
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177 Another source of weakness is t
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179 PLATING IN A CORONA DISCHARGE R
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\ 3 , ,\ 110 v 60 CPS MANOMETER . F
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I i , \ I i & a - P Fig. 3 Reaction
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\ \' C 0 .d * d .- C U d 0) c( 1) L
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I i I . Q) I, s w 0 v) Y 0 a w W a
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I (b) Polarized Light Fig. 6 Cross
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i m v) Y C i! u o) 23 a a- + 191 m
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i, d C .d c c W Q ) 0 0 L1Y 0 000 0
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i e 4 0 wcr -4 4 al 0 0 0 c) cr 13:
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\ E ‘ 1 TIME FOR RUN 13-1 14-1 -
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199 a red heat in this cell using d
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\ , t j \ I, v) 2 Y . C 0 u m .I C
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203 VAPOR PHASE FORMATION OF NONCRY
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BELL JAR STANC TO VACUUM SYSTEM U T
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207 of the boron oxide film, the fi
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i I, 4 I.( Y I- * 0 i f i 3 0.t I I
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211 The Reacticn 3f Oxygen with Car
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2 E, W t- a Z 9 I- a 2 X 0 I50 too
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'i' 100 50 IC 21 5 2.0 2.5 SURFACE
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I- z W 0 w a a 100 80 60 40 20 215
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s., Literature Cited Berkley, C. ,
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7 h \ F 221 600°C and 1 atmosphere
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223 e I'
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R L ' -1 9mm O.D. 5mm I.D. 45mm 0.D
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Figure 5.- Paschen's law curves. 2-
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\ '? I The water-free product gases
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N I + 0" ON i I + 0 u / 0 0 I 0 cu
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- 233 SOME PROBLEMS OF THE KINETICS
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.. . :. ,. .I , . i ? .. . , ... .
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237 Table 2 Experimental Variables
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239 Zhbie I Eerccnt Consumption of
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241 Discussion The systematic varia
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I \ 1 243 FORMATION OF HYDROCARBONS
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h z - a o m a 20 T IME, minutes . F
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I 1 I I I I 0 I 2 3 4 5 TIME, minut
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The next five coluws in table 1 sho
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\ .\ t 251 Given the existence of t
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I L 253 Epple, R. P. and C. M. Apt.
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1 ' Fig. 1 Schematic of flow discha
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5' . ' I 1 257 co, with excess H2,
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1 1 1 moo 1400 1300 c V' I IPOO I I
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i 25i The Dlssocfatior of ToIuere V
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L ! , c PRODUCTS FROM A 28 MC. DISC
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'\ J ?. , .. . : PRODUCT FORMATION
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'9 / I '\ "1 BENZYL CATION AND RADI
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a
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271 tube serve? as the high voltare
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273 ion (1L.). Zxcitei-ion by colli
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Apparatus and Procedure 275 EXPERIM
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. 277 6. A freshly prepared sam le
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observed. The polystyrene (10% solu
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i i (12) c (11) (14) I 281 LITERATU
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FLOW- METER I ADDITIVE SUPPLY * ,28
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285 TABLE 2 Effect of Haloqenated A
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ANALYTICAL RESULTS Some evidence wa
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DISCUSSION 289 The salient features
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? ~ MENBERSHIP IN THE DIVISION OF F
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292 flow of the reactant gas stream
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294 have suitable residence times i
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0 E < h( E l! d K c 0 .- Y 0 t u t
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298 yields of many chemical product
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- ;i Y . 15. Pressure lOmm 5 > 10-
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302 the best and in many practical
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GENERATION AND MEASUREMENT OF AUDIO
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. The transformer secondary and the
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Vaccum-Tube Amplifier The mobile co
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310 f = Power supply frequency in c
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FUFARCI! INSTITUTE OF TFYDLC UNIVER
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J # I / 4) I . . '8 r4 0 r( P
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317 i Cuencb svsten w.nnar;itus use
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epcrte? the noss~kil.itv of nroduct
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1' b t +
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323 ....... - . . . . . . . . . . .
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1 \ i I i , / / / 8 3 1 325 To205 +
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- .- - - . - - . . . - . 327 n + c
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' POWER PLASMA GAS l e , ' I ! I I
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331 f'ENI?AL PF'FCLCCFC Dernis, P.R
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i J 333 ; mosphere (as opposed to a
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; it raised the question, still &?z
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p .I V I .= - - HCN/C(CALC. WITH C
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1 1 339 atmospheric ressure and ach
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RESULTS 341 Composition Dependence
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0.09 0.08 0.07 9 0.06 2 U - .$ 0.05
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II \ to the Slot So that less of th
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i 4 2 HYDROCARBON-NITROGEN REACTION
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I 1 349 c M m ; a e, k M x
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1.0 I - a. I n TEMPERATURE - OK Fig
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353 the experimental results in the
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,) 355 The ceaswed conversion cf ni
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1 6 357 Freezing. 3jpotnesise thzf
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359 \ Frozen Compositior: Calcillat
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I 1 \ 361 -. ne reaction proceecis
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\ 36 3 ' h, I 26. H. Purnell, Gas C
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In experiments on the direct conver
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367 used as blnders, with different
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369 ' i 1. REFERENCES Berber, John
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Distribution and yield rates of pro
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. . I . I 370 . . . . ., . . .. . .
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4 372 090- > E w - m c N O - 0 z :
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A-Feed tank 6-Thermocracker GReceiv
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80 \ 0 70 60 e 40 a U VI 9 30 20 10
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COAL DEASH& AND HIGH-PURITY COKE Wa
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3Pn _. -. - L -J:,J.-;~~~L, ):as se
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S ~ l ~ o n~pg:ading r is the resul
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The range ~f temperatures and gener
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. .. 386 9 * - r. Y 2 .' d a f' r.
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.) .L m 388 I
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TABLE 4 390 DELAYED COKING OF DEASH
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, ! I- on '---
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394 The present method is to keep t
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396 ‘c erperature, while the pres
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2, '! ! Proximate Analysis, wt $ Mo
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0 IS 0 14 LL 9 013 e \ 3 b- m *- 01
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402 HYDROGEN CYANIDE PRODUCED FROM
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404 Before startup, the system is p
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4 OL. ' , I. . TesCs. With.Coals .o
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Table 3.- Product Gas Analyses and
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410 BIBLIOGRAPHY 1. American Public
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Figure 2. Enclosure surrounding hyd
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0 0 f v) C 0 u m I z 2 c 2 r d J w
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0. E c .4 7 .. .c . I ( - Low tempe
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418 cual. A mjor aa\;antage or' the
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420 Ir ?Y ? ? 9 9 9 pc rod n o c o
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422 Table 3. Room-texperature M'dss
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424 state, depending on the strengt
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Table 4. Room-?;ergerature isomer s
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I' 1.3 . /o 9 IO 9 6 a 425 F F 33 I
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Brooks J.D. and Sternhell S. (1957)
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(52) Gib3 T.C. and Greenwood N.N. (
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434 transducer vas then introduced
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436 yield is quite similar. The con
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?-!??? 0 mv, Uh\OhIe . . . . eirlrl
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4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 4
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442 CHEMICAL REACTIONS IN A CORONA
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helium 444 CORONA REACTOR SYSTEM Fi
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446 The ultraviolet spectrum. for t
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Biphenyl Fraction 448 The low molec
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LUd The actual structural definitio
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I I I I I In m 9 In 2 , I: r- In m
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’. 454 Mechanism I The available
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456 , , . The relatively low yield
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458 h/lethylacetylene, allene and b
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Introduction VAPOR PHASE DECOMPOSIT
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462 more efficient hydrogenation. T
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464 place in parallel with fragment
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466 P rl 0, k 7 rnI rn al k a I hl
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458 TABLE I. COMPOSI'IION OF GASEOU
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REFERENCES 1. C. Hirayama and D. A.
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i 472 Reciprocal Arc Enthalpy ,-> F
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474 be pumped down without altering
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476 Instead a hydrogen deficient fi
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i 478
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480 FATTY ACIDS AND n-ALKANES IN GR
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482 TA5L,E 2. - Carbon number distr
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6. 7. a. 9. 484 Lawlor, D. L., and
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' I ' Sample No. 6 ' 12 IO 8 6 z 4
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. 488 uiolecular weight of which ca
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Xississippi (Sample GS). Stock solu
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492 found at 5.7 and 4.9& for the W
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494 mechanisms. However, the voltad
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For pure polynuclcar arom.i;ic hydr
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- '-'. . ' . . values are listed in
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500 (1;) Ten, T. 17.: a;1d,Dic;
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- ~ Resistivity Czlculation 2: 1 j:
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504 o ' C 0s 2 0 v x i 8 2 0 ! P -
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506 i
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d 601 L P LL
Page 516 and 517: I I I I I I I I m W N W N 0 (D ? 0
Page 518 and 519: 514 was heated under nitrogen in a
Page 520 and 521: The line broadening at 79OK of the
Page 522 and 523: 13. 14. 15. 16. 17. 18. 19. 20. 21.
Page 524 and 525: W L, Z 6 m (1: 0 6 d j o 2 ' 1 0.0
Page 526 and 527: Coals 522 Studies of the 1600 cm-l
Page 528 and 529: L in ole i c a c id - 0' Two sample
Page 530 and 531: 526 Table 1.- Ultimate analyses of
Page 532 and 533: 528 6. Friedel, R. A., and H. Retco
Page 534 and 535: egeneration. The system can be seen
Page 536 and 537: 532 and can be expressed in terms o
Page 538 and 539: 534 in the vapor increases with inc
Page 540 and 541: NH3 NH3 NH3 NH3 Pyridine Pyridine P
Page 542 and 543: Mole Ratio of Test No. Quinoline to
Page 544 and 545: IXPROFJCTION D; M. Mason Institute
Page 546 and 547: -4:c~rciiny to recent studies o ;i4
Page 548 and 549: 544 Table 1. LIGHT EMISSION OF Y"TR
Page 550 and 551: emission in a few cases may be by d
Page 552 and 553: LITERATUR2 CITED i. C. -. .' * il.
Page 554 and 555: co, CH,,OR 1 - OTHER ADDITIVE FRITT
Page 556 and 557: FRIT 'TED CO, CH,.OR 4 ___ OTHER AD
Page 558 and 559: 340 350 300 400 4 50 500 600 700 80
Page 560 and 561: 0 554 WITH COOLING (PLATE AT 40°C)
Page 562 and 563: 5 56 then t = to when e = 0 2) the
Page 564 and 565: 5 58 The surface heat transfer coef
Page 568 and 569: __- ._ 562 Table I THERMAL AND PHYS
Page 570: ln 4 I 0 4J v \ 1.0 0.8 0.6 L - 0.4
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