EXPLANATION OF TABLE II.

38. The calculation of the mechanical effect, in any case, which might

always be effected in the manner described in § 37 (with the proper

modification for fractions of degrees, when necessary), is much

simplified by the use of Table II., where the first number of Table I.,

the sum of the first and second, the sum of the first three, the sum of

the first four, and so on, are successively exhibited. The sums thus

tabulated are the values of the integrals

∫_{0}^1 μ_dt_, ∫_{0}^2 μ_dt_, ∫_{0}^3 μ_dt_, ... ∫_{0}^{231} μ_dt_;

and, if we denote ∫_{0}^t μ_dt_ by the letter _M_, Table II. may be

regarded as a table of the value of _M_.

_To find the amount of mechanical effect due to a unit of heat

descending from a body at a temperature S to a body at T, if these

numbers be integers, we have merely to subtract the value of M, for the

number T, from the value for the number S, given in Table II._

TABLE I.[56]

MEAN VALUES OF Μ FOR THE SUCCESSIVE DEGREES OF THE AIR-THERMOMETER FROM

0° TO 230°.

───────────────────────────────────┬───────────────────────────────────

° │ μ

───────────────────────────────────┼───────────────────────────────────

1│ 4.960

2│ 4.946

3│ 4.932

4│ 4.918

5│ 4.905

6│ 4.892

7│ 4.878

8│ 4.865

9│ 4.852

10│ 4.839

11│ 4.826

12│ 4.812

13│ 4.799

14│ 4.786

15│ 4.773

16│ 4.760

17│ 4.747

18│ 4.735

19│ 4.722

20│ 4.709

21│ 4.697

22│ 4.684

23│ 4.672

24│ 4.659

25│ 4.646

26│ 4.634

27│ 4.621

28│ 4.609

29│ 4.596

30│ 4.584

31│ 4.572

32│ 4.559

33│ 4.547

34│ 4.535

35│ 4.522

36│ 4.510

37│ 4.498

38│ 4.486

39│ 4.474

40│ 4.462

41│ 4.450

42│ 4.438

43│ 4.426

44│ 4.414

45│ 4.402

46│ 4.390

47│ 4.378

48│ 4.366

49│ 4.355

50│ 4.343

51│ 4.331

52│ 4.319

53│ 4.308

54│ 4.296

55│ 4.285

56│ 4.273

57│ 4.262

58│ 4.250

59│ 4.239

60│ 4.227

61│ 4.216

62│ 4.205

63│ 4.194

64│ 4.183

65│ 4.172

66│ 4.161

67│ 4.150

68│ 4.140

69│ 4.129

70│ 4.119

71│ 4.109

72│ 4.098

73│ 4.088

74│ 4.078

75│ 4.067

76│ 4.057

77│ 4.047

78│ 4.037

79│ 4.028

80│ 4.018

81│ 4.009

82│ 3.999

83│ 3.990

84│ 3.980

85│ 3.971

86│ 3.961

87│ 3.952

88│ 3.943

89│ 3.934

90│ 3.925

91│ 3.916

92│ 3.907

93│ 3.898

94│ 3.889

95│ 3.880

96│ 3.871

97│ 3.863

98│ 3.854

99│ 3.845

100│ 3.837

101│ 3.829

102│ 3.820

103│ 3.812

104│ 3.804

105│ 3.796

106│ 3.788

107│ 3.780

108│ 3.772

109│ 3.764

110│ 3.757

111│ 3.749

112│ 3.741

113│ 3.734

114│ 3.726

115│ 3.719

116│ 3.712

117│ 3.704

118│ 3.697

119│ 3.689

120│ 3.682

121│ 3.675

122│ 3.668

123│ 3.661

124│ 3.654

125│ 3.647

126│ 3.640

127│ 3.633

128│ 3.627

129│ 3.620

130│ 3.614

131│ 3.607

132│ 3.601

133│ 3.594

134│ 3.586

135│ 3.579

136│ 3.573

137│ 3.567

138│ 3.561

139│ 3.555

140│ 3.549

141│ 3.543

142│ 3.537

143│ 3.531

144│ 3.525

145│ 3.519

146│ 3.513

147│ 3.507

148│ 3.501

149│ 3.495

150│ 3.490

151│ 3.484

152│ 3.479

153│ 3.473

154│ 3.468

155│ 3.462

156│ 3.457

157│ 3.451

158│ 3.446

159│ 3.440

160│ 3.435

161│ 3.430

162│ 3.424

163│ 3.419

164│ 3.414

165│ 3.409

166│ 3.404

167│ 3.399

168│ 3.394

169│ 3.389

170│ 3.384

171│ 3.380

172│ 3.375

173│ 3.370

174│ 3.365

175│ 3.361

176│ 3.356

177│ 3.351

178│ 3.346

179│ 3.342

180│ 3.337

181│ 3.332

182│ 3.328

183│ 3.323

184│ 3.318

185│ 3.314

186│ 3.309

187│ 3.304

188│ 3.300

189│ 3.295

190│ 3.291

191│ 3.287

192│ 3.282

193│ 3.278

194│ 3.274

195│ 3.269

196│ 3.265

197│ 3.261

198│ 3.257

199│ 3.253

200│ 3.249

201│ 3.245

202│ 3.241

203│ 3.237

204│ 3.233

205│ 3.229

206│ 3.225

207│ 3.221

208│ 3.217

209│ 3.213

210│ 3.210

211│ 3.206

212│ 3.202

213│ 3.198

214│ 3.195

215│ 3.191

216│ 3.188

217│ 3.184

218│ 3.180

219│ 3.177

220│ 3.173

221│ 3.169

222│ 3.165

223│ 3.162

224│ 3.158

225│ 3.155

226│ 3.151

227│ 3.148

228│ 3.144

229│ 3.141

230│ 3.137

231│ 3.134

───────────────────────────────────┴───────────────────────────────────

TABLE II.

MECHANICAL EFFECT IN FOOT-POUNDS DUE TO A THERMIC UNIT CENTIGRADE,

PASSING FROM A BODY, AT ANY TEMPERATURE LESS THAN 230° TO A BODY AT 0°.

───────────────────────────────────┬───────────────────────────────────

Superior Limit of Temperature. │ Mechanical Effect.

───────────────────────────────────┼───────────────────────────────────

° │ Ft.-Pounds.

│

1│ 4.960

2│ 9.906

3│ 14.838

4│ 19.756

5│ 24.661

6│ 29.553

7│ 34.431

8│ 39.296

9│ 44.148

10│ 48.987

11│ 53.813

12│ 58.625

13│ 63.424

14│ 68.210

15│ 72.983

16│ 77.743

17│ 82.490

18│ 87.225

19│ 91.947

20│ 96.656

21│ 101.353

22│ 106.037

23│ 110.709

24│ 115.368

25│ 120.014

26│ 124.648

27│ 129.269

28│ 133.878

29│ 138.474

30│ 143.058

31│ 147.630

32│ 152.189

33│ 156.736

34│ 161.271

35│ 165.793

36│ 170.303

37│ 174.801

38│ 179.287

39│ 183.761

40│ 188.223

41│ 192.673

42│ 197.111

43│ 201.537

44│ 205.951

45│ 210.353

46│ 214.743

47│ 219.121

48│ 223.487

49│ 227.842

50│ 232.185

51│ 236.516

52│ 240.835

53│ 245.143

54│ 249.439

55│ 253.724

56│ 257.997

57│ 262.259

58│ 266.509

59│ 270.748

60│ 274.975

61│ 279.191

62│ 283.396

63│ 287.590

64│ 291.773

65│ 295.945

66│ 300.106

67│ 304.256

68│ 308.396

69│ 312.525

70│ 316.644

71│ 320.752

72│ 324.851

73│ 328.939

74│ 333.017

75│ 337.084

76│ 341.141

77│ 345.188

78│ 349.225

79│ 353.253

80│ 357.271

81│ 361.280

82│ 365.279

83│ 369.269

84│ 373.249

85│ 377.220

86│ 381.181

87│ 385.133

88│ 389.076

89│ 393.010

90│ 396.935

91│ 400.851

92│ 404.758

93│ 408.656

94│ 412.545

95│ 416.425

96│ 420.296

97│ 424.159

98│ 428.013

99│ 431.858

100│ 435.695

101│ 439.524

102│ 443.344

103│ 447.156

104│ 450.960

105│ 454.756

106│ 458.544

107│ 462.324

108│ 466.096

109│ 469.860

110│ 473.617

111│ 477.366

112│ 481.107

113│ 484.841

114│ 488.567

115│ 492.286

116│ 495.998

117│ 499.702

118│ 503.399

119│ 507.088

120│ 510.770

121│ 514.445

122│ 518.113

123│ 521.174

124│ 525.428

125│ 529.075

126│ 532.715

127│ 536.348

128│ 539.975

129│ 543.595

130│ 547.209

131│ 550.816

132│ 554.417

133│ 558.051

134│ 561.597

135│ 565.176

136│ 568.749

137│ 572.316

138│ 575.877

139│ 579.432

140│ 582.981

141│ 586.524

142│ 590.061

143│ 593.592

144│ 597.117

145│ 600.636

146│ 604.099

147│ 607.656

148│ 611.157

149│ 614.652

150│ 618.142

151│ 621.626

152│ 625.105

153│ 628.578

154│ 632.046

155│ 635.508

156│ 638.965

157│ 642.416

158│ 645.862

159│ 649.302

160│ 652.737

161│ 656.167

162│ 659.591

163│ 663.010

164│ 666.424

165│ 669.833

166│ 673.237

167│ 676.636

168│ 680.030

169│ 683.419

170│ 686.803

171│ 690.183

172│ 693.558

173│ 696.928

174│ 700.293

175│ 703.654

176│ 707.010

177│ 710.361

178│ 713.707

179│ 717.049

180│ 720.386

181│ 723.718

182│ 727.046

183│ 730.369

184│ 733.687

185│ 737.001

186│ 740.310

187│ 743.614

188│ 746.914

189│ 750.209

190│ 753.500

191│ 756.787

192│ 760.069

193│ 763.347

194│ 766.621

195│ 769.890

196│ 773.155

197│ 776.416

198│ 779.673

199│ 782.926

200│ 786.175

201│ 789.420

202│ 792.661

203│ 795.898

204│ 799.131

205│ 802.360

206│ 805.585

207│ 808.806

208│ 812.023

209│ 815.236

210│ 818.446

211│ 821.652

212│ 824.854

213│ 828.052

214│ 831.247

215│ 834.438

216│ 837.626

217│ 840.810

218│ 843.990

219│ 847.167

220│ 850.340

221│ 853.509

222│ 856.674

223│ 859.836

224│ 862.994

225│ 866.149

226│ 869.300

227│ 872.448

228│ 875.592

229│ 878.733

230│ 881.870

231│ 885.004

───────────────────────────────────┴───────────────────────────────────

_Note on the curves described in Clapeyron’s graphical method of

exhibiting Carnot’s Theory of the Steam-Engine._

39. At any instant when the temperature of the water and vapor is _t_,

during the fourth operation (see above, § 16, and suppose, for the sake

of simplicity, that at the beginning of the first and at the end of the

fourth operation the piston is absolutely in contact with the surface of

the water), the latent heat of the vapor must be precisely equal to the

amount of heat that would be necessary to raise the temperature of the

whole mass, if in the liquid state, from _t_ to _S_.[57] Hence, if _v′_

denote the volume of the vapor, _c_ the mean capacity for heat of a

pound of water between the temperatures _S_ and _t_, and _W_ the weight

of the entire mass, in pounds, we have

_kv′_ = _c_(_S_ − _t_)_W_.

Again, the circumstances during the second operation are such that the

mass of liquid and vapor possesses _H_ units of heat more than during

the fourth; and consequently, at the instant of the second operation,

when the temperature is _t_, the volume _v_ of the vapor will exceed

_v′_ by an amount of which the latent heat is _H_, so that we have

_v_ = _v′_ + (_H_)/(_k_).

40. Now, at any instant, the volume between the piston and its primitive

position is less than the actual volume of vapor by the volume of the

water evaporated. Hence, if _x_ and _x′_ denote the abscissæ of the

curve at the instants of the second and fourth operations respectively,

when the temperature is _t_, we have

_x_ = _v_ − σ_v_, _x′_ = _v′_ − σ_v′_,

and, therefore, by the preceding equations,

_x_ = (1 − σ)/(_k_){_H_ + _c_(_S_ − _t_)_W_}, (_a_)

_x′_ = (1 − σ)/(_k_)_c_(_S_ − _t_)_W_. (_b_)

These equations, along with _y_ = _y′_ = _p_, (_c_)

enable us to calculate, from the data supplied by Regnault, the abscissa

and ordinate for each of the curves described above (§ 17) corresponding

to any assumed temperature _t_. After the explanations of §§ 33, 34, 35,

36, it is only necessary to add that _c_ is a quantity of which the

value is very nearly unity, and would be exactly so were the capacity of

water for heat the same at every temperature as it is between 0° and 1°;

and that the value of _c_(_S_ − _t_), for any assigned values of _S_ and

_t_, is found, by subtracting the number corresponding to _t_ from the

number corresponding to _s_, in the column headed “_Nombre des unités de

chaleur abandonnées par un kilogramme d’eau en descendant de T° à 0°_,”

of the last table (at the end of the tenth memoir) of Regnault’s work.

By giving _S_ the value 230°, and by substituting successively 220, 210,

200, etc., for _t_, values for _x_, _y_, _x′_, _y′_, have been found,

which are exhibited in the table opposite.

─────────────┬─────────────────┬────────────────────────┬─────────────

Temperatures.│ Volumes to be │ Volumes from the │Pressures of

│described by the │ primitive position of │ saturated

│ piston, to │ the piston to those │ steam, in

│ complete the │occupied at instants of │pounds on the

│fourth operation.│ the second operation. │square foot.

_t_ │ _x′_ │ _x_ │_y_ = _y′_ =

│ │ │ _p_

─────────────┼─────────────────┼────────────────────────┼─────────────

0°│ 1269. _W_ │_x′_ + 5.409._H_ │ 12.832

10│ 639.6. _W_ │_x′_ + 2.847._H_ │ 25.567

20│ 337.3. _W_ │_x′_ + 1.571._H_ │ 48.514

30│ 185.5. _W_ │_x′_ + .9062._H_ │ 88.007

40│ 105.9. _W_ │_x′_ + .5442._H_ │ 153.167

50│ 62.62. _W_ │_x′_ + .3392._H_ │ 256.595

60│ 38.19. _W_ │_x′_ + .2188._H_ │ 415.070

70│ 21.94. _W_ │_x′_ + .1456._H_ │ 650.240

80│ 15.38. _W_ │_x′_ + .09962._H_ │ 989.318

90│ 10.09. _W_ │_x′_ + .06994._H_ │ 1465.80

100│ 6.744. _W_ │_x′_ + .05026._H_ │ 2120.11

110│ 4.578. _W_ │_x′_ + .03688._H_ │ 2999.87

120│ 3.141. _W_ │_x′_ + .02758._H_ │ 4160.10

130│ 2.176. _W_ │_x′_ + .02098._H_ │ 5663.70

140│ 1.519. _W_ │_x′_ + .01625._H_ │ 7581.15

150│ 1.058. _W_ │_x′_ + .01271._H_ │ 9990.26

160│ 0.7369. _W_ │_x′_ + .01010._H_ │ 12976.2

170│ 0.5085. _W_ │_x′_ + .008116._H_ │ 16630.7

180│ 0.3454. _W_ │_x′_ + .006592._H_ │ 21051.5

190│ 0.2267. _W_ │_x′_ + .005406._H_ │ 26341.5

200│ 0.1409. _W_ │_x′_ + .004472._H_ │ 32607.7

210│ 0.0784. _W_ │_x′_ + .003729._H_ │ 39960.7

220│ 0.3310. _W_ │_x′_ + .003130._H_ │ 48512.4

230│ 0 │_x′_ + .002643._H_ │ 58376.6

─────────────┴─────────────────┴────────────────────────┴─────────────

_Appendix._

(Read April 30, 1849.)

41. In p. 30 some conclusions drawn by Carnot from his general reasoning

were noticed; according to which it appears, that if the value of μ for

any temperature is known, certain information may be derived with

reference to the saturated vapor of any liquid whatever, and, with

reference to any gaseous mass, without the necessity of experimenting

upon the specific medium considered. Nothing in the whole range of

Natural Philosophy is more remarkable than the establishment of general

laws by such a process of reasoning. We have seen, however, that doubt

may exist with reference to the truth of the axiom on which the entire

theory is founded, and it therefore becomes more than a matter of mere

curiosity to put the inferences deduced from it to the test of

experience. The importance of doing so was clearly appreciated by

Carnot; and, with such data as he had from the researches of various

experimenters, he tried his conclusions. Some very remarkable

propositions which he derives from his theory coincide with Dulong and

Petit’s subsequently discovered experimental laws with reference to the

heat developed by the compression of a gas; and the experimental

verification is therefore in this case (so far as its accuracy could be

depended upon) decisive. In other respects, the data from experiment

were insufficient, although, so far as they were available as tests,

they were confirmatory of the theory.

42. The recent researches of Regnault add immensely to the experimental

data available for this object, by giving us the means of determining

with considerable accuracy the values of μ within a very wide range of

temperature, and so affording a trustworthy standard for the comparison

of isolated results at different temperatures, derived from observations

in various branches of physical science.

In the first section of this Appendix the theory is tested, and shown to

be confirmed by the comparison of the values of μ found above, with

those obtained by Carnot and Clapeyron from the observations of various

experimenters on air, and the vapors of different liquids. In the second

and third sections some striking confirmations of the theory arising

from observations by Dulong, on the specific heat of gases, and from Mr.

Joule’s experiments on the heat developed by the compression of air, are

pointed out; and in conclusion, the actual methods of obtaining

mechanical effect from heat are briefly examined with reference to their

economy.

I. _On the values of μ derived by Carnot and Clapeyron from observations

on Air, and on the Vapors of various liquids._

43. In Carnot’s work, pp. 80–82, the mean value of μ between 0° and 1°

is derived from the experiments of Delaroche and Bérard on the specific

heat of gases, by a process approximately equivalent to the calculation

of the value of (_Ep_{0}v_{0}_)/(_vdq_/_dv_) for the temperature ½°.

There are also, in the same work, determinations of the values of μ from

observations on the vapors of alcohol and water; but a table given in M.

Clapeyron’s paper, of the values of μ derived from the data supplied by

various experiments with reference to the vapors of ether, alcohol,

water, and oil of turpentine, at the respective boiling-points of these

liquids, affords us the means of comparison through a more extensive

range of temperature. In the cases of alcohol and water, these results

ought of course to agree with those of Carnot. There are, however,

slight discrepancies which must be owing to the uncertainty of the

experimental data.[58] In the opposite table, Carnot’s results with

reference to air, and Clapeyron’s results with reference to the four

different liquids, are exhibited, and compared with the values of μ

which have been given above (Table I.) for the same temperatures, as

derived from Regnault’s observations on the vapor of water.

────────────┬──────────────┬──────────────┬──────────────┬─────────────

│ │ │ Values of μ │

│ │ │ deduced from │

Names of the│ │ │ Regnault’s │

Media. │Temperatures. │ Values of μ. │Observations. │Differences.

────────────┼──────────────┼──────────────┼──────────────┼─────────────

│ ° │ (Carnot) │ │

Air │ 0.5│ 4.377│ 4.960│ .383

Sulphuric │ (Boil. pt.)│ (Clapeyron)│ │

Ether │ 35.5│ 4.478│ 4.510│ .032

Alcohol │ 78.8│ 3.963│ 4.030│ .071

Water │ 100│ 3.658│ 3.837│ .179

Essence of │ │ │ │

Turpentine│ 156.8│ 3.530│ 3.449│ −.081

────────────┴──────────────┴──────────────┴──────────────┴─────────────

44. It may be observed that the discrepancies between the results

founded on the experimental data supplied by the different observers

with reference to water at the boiling-point, are greater than those

which are presented between the results deduced from any of the other

liquids, and water at the other temperatures; and we may therefore feel

perfectly confident that the verification is complete to the extent of

accuracy of the observations.[59] The considerable discrepancy presented

by Carnot’s result deduced from experiments on air, is not to be

wondered at when we consider the very uncertain nature of his data.

45. The fact of the gradual decrease of μ through a very extensive range

of temperature, being indicated both by Regnault’s continuous series of

experiments and by the very varied experiment on different media, and in

different branches of Physical Science, must be considered as a striking

verification of the theory.

Reflections on the motive power of heat · 第 27 / 44 题