Untitled - Aerobib - Universidad Politécnica de Madrid

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13.16. APPENDIX: APPLICATION OF PROBERT’S METHOD 335 [21] Godsave, G. A.: The Burning of Single Drops of Fuel. Part. I, Temperature Distribution and Heat Transfer in the Preflame Region. NGTE Report no. R.66, 1950. Part II, Experimental Results. NGTE Report no. 87, 1951. Part III, Comparison of Theoretical and Experimental Burning Rates and Discussion of the Mechanism of the Combustion Process. NGTE Report no. R.38, 1952. [22] Topps, J. E. C.: An Experimental Study of the Evaporation and Combustion of Falling Droplets. Journal of the Institute of Petroleum, 1951, pp. 535-537. [23] Hall, L. R. and Die<strong>de</strong>richsen, J.: An Experimental Study of the Burning of Single Drops of Fuel in Air at Pressures up to Twenty Atmospheres. Fourth Symposium (International) on Combustion, Williams and Wilkins Co., Baltimore, 1953, pp. 837-846. [24] Spalding, D. B. Combustion of Single Droplet and of a Fuel Spray. Selected Combustion Problems, Vol. I, AGARD, 1954, pp. 340-351. [25] Hottel, H. C., Williams, G. C. and Simpson, H. C.: The Combustion of Droplets of Heavy Liquid Fuels. Fifth Symposium (International) on Combustion, Reinhold Publishing Corp., New York, 1955, pp. 101-129. [26] Wise, H., Lowell, J, and Wood, B. J.: The Effects of Chemical and Physical Parameters on the Burning Rate of a Liquid Droplet. Fifth Symposium (International) on Combustion, Reinhold Publishing Corp., New York, 1955, pp. 132- 141. [27] Kobayasi, K.: An Experimental Study on the Combustion of a Fuel Droplet. Fifth Symposium (International) on Combustion, Reinhold Publishing Corp., New York, 1955, pp. 141-148. [28] Nischiwali, N.: Kinetics of Liquid Combustion Processes: I. Evaporation and Ignition Lag of Fuel Droplets. Fifth Symposium (International) on Combustion, Reinhold Publishing Corp., New York, 1955, pp. 148-158. [29] Surugue, J.: Combustion Problems in Turbojets. AGARD AG 5/P2, December 1952, pp. 54-61. [30] Bahr, D.: Evaporation and Spreading of Isooctane Sprays in High-Velocity Air Streams. NACA RM E511 E53114, 1953. [31] Saks, W.: The Rate of Evaporation of a Kerosene Spray. National Aeronautical Institute of Canada, Note No. 7, 1951. [32] Frössling, N.: On the Evaporation of Falling Drops. Gerlands Beiträge zur Geophysik, 1938, pp. 170-216. [33] Ranz, W. E. and Marshall, W. R.: Evaporation from Drops. Chemical Engineering Progress, 1952, pp. 141-46 and 173-180.
336 CHAPTER 13. COMBUSTION OF LIQUID FUELS [34] Ingebo, R. D.: Vaporization Rates and Heat-Transfer Coefficients for Pure Liquid Drops. NACA Tech. Note No. 2368, 1951. [35] Miesse C. C.: Ballistics of an Evaporating Droplet. Jet Propulsion, July-August 1954, pp. 237-244. [36] Penner, S. S.: On Maximum Evaporation Rates of Liquid Droplet in Rocket Motors. Journal of the American Rocket Society, March-April 1953, pp. 85-88.
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Aerothermochemistry Gregorio Millá
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PRESENTACIÓN Amable Liñán Es un
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que no cambiaron los resultados, y
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INSTITUTO NACIONAL DE TÉCNICA AERO
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aim to become acquainted with Aerot
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Tarifa, Manuel de Sendagorta and Ig
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3.4 Energy equation . . . . . . . .
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8.4 Quenching . . . . . . . . . . .
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Chapter 1 Thermochemistry 1.1 Intro
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1.1. INTRODUCTION 3 GAS ε/k (K) σ
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1.1. INTRODUCTION 5 14 12 10 N 2 CH
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1.2. THERMODYNAMIC FUNCTIONS OF AN
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1.2. THERMODYNAMIC FUNCTIONS OF AN
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1.3. MIXTURE OF GASES 11 Helmholtz
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1.3. MIXTURE OF GASES 13 is the par
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1.3. MIXTURE OF GASES 15 Entropy Si
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1.4. CALCULATION OF THE THERMODYNAM
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1.4. CALCULATION OF THE THERMODYNAM
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1.5. CHEMICAL REACTIONS IN A MIXTUR
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1.6. CHEMICAL EQUILIBRIUM 23 Since
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∆G 0 j = ∑ i 1.7. CASE OF A MIX
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1.7. CASE OF A MIXTURE OF IDEAL GAS
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1.8. CHEMICAL KINETICS 29 1.8 Chemi
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1.8. CHEMICAL KINETICS 31 Mechanics
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1.8. CHEMICAL KINETICS 33 This stru
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1.8. CHEMICAL KINETICS 35 [3] Hirsc
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Chapter 2 Transport phenomena in ga
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2.2. DIFFUSION 39 Hereinafter, nota
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2.2. DIFFUSION 41 where r is the di
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2.2. DIFFUSION 43 T ∗ Ω (1,1)∗
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2.2. DIFFUSION 45 Gas Pair σ 12 (
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2.2. DIFFUSION 47 coefficients. 14
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2.3. VISCOSITIES 49 2.3 Viscosities
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2.3. VISCOSITIES 51 Here µ and µ
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2.3. VISCOSITIES 53 Its value depen
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2.4. THERMAL CONDUCTIVITY 55 2000 1
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2.4. THERMAL CONDUCTIVITY 57 4000 3
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Chapter 3 General equations 3.1 Int
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3.2. EQUATION OF CONTINUITY 61 The
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3.2. EQUATION OF CONTINUITY 63 A i
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3.4. ENERGY EQUATION 65 where the s
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3.4. ENERGY EQUATION 67 The energy
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3.5. GENERAL EQUATIONS 69 obtained
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3.6. ENTROPY VARIATION 71 Taking in
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3.7. ONE-DIMENSIONAL MOTIONS 73 red
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3.8. STATIONARY, ONE-DIMENSIONAL MO
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3.9. THE CASE OF ONLY TWO CHEMICAL
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3.10. STATIONARY, ONE-DIMENSIONAL M
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3.11. APPENDIX: NOTATION AND REPERT
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3.11. APPENDIX: NOTATION AND REPERT
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Chapter 4 Combustion Waves 4.1 Deto
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4.2. KINDS OF DETONATIONS AND DEFLA
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4.2. KINDS OF DETONATIONS AND DEFLA
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4.3. VELOCITY OF THE BURNT GASES 95
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4.3. VELOCITY OF THE BURNT GASES 97
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4.4. PROPAGATION VELOCITY 99 p H’
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4.5. APPLICATIONS 101 By substituti
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4.7. INDETERMINACY OF THE SOLUTION
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Chapter 5 Structure of the combusti
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5.2. WAVE EQUATIONS 107 of diffusio
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5.2. WAVE EQUATIONS 109 2) Burnt ga
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5.4. LIMITING FORM OF THE WAVE EQUA
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5.4. LIMITING FORM OF THE WAVE EQUA
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5.5. DETONATIONS 115 Of these two v
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5.5. DETONATIONS 117 waves. Such th
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5.5. DETONATIONS 119 This relation
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5.5. DETONATIONS 121 curves, repres
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5.6. DEFLAGRATIONS 123 mum temperat
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5.6. DEFLAGRATIONS 125 8 7 v/v 1 =T
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5.7. TRANSITION FROM DEFLAGRATION T
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5.7. TRANSITION FROM DEFLAGRATION T
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Chapter 6 Laminar flames 6.1 Introd
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6.1. INTRODUCTION 133 papers presen
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6.3. BOUNDARY CONDITIONS 135 c) Dif
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6.4. MODIFICATION OF THE CONDITIONS
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6.4. MODIFICATION OF THE CONDITIONS
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6.6. EXAMPLE 141 generally impossib
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6.6. EXAMPLE 143 Two more relations
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6.7. REACTION VELOCITY 145 1.0 0.8
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6.8. FLAME EQUATIONS 147 6.8 Flame
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6.9. SOLUTION OF THE FLAME EQUATION
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6.10. STRUCTURE OF THE COMBUSTION W
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6.11. IGNITION TEMPERATURE 161 6.11
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6.12. GENERAL EQUATIONS FOR THE COM
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6.13. OZONE DECOMPOSITION FLAME 169
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6.14. HYDRAZINE DECOMPOSITION FLAME
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6.15. FLAME PROPAGATION IN HYDROGEN
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Chapter 7 Turbulent flames 7.1 Intr
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7.1. INTRODUCTION 209 300 250 TURBU
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7.2. TURBULENT COMBUSTION THEORIES
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7.4. COMPARISON WITH EXPERIMENTAL R
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Chapter 8 Ignition, flammability an
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8.2. IGNITION 223 comparison betwee
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8.3. FLAMMABILITY LIMITS 225 The pr
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8.4. QUENCHING 227 8.4 Quenching So
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8.4. QUENCHING 229 [19] Simon, D. M
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Chapter 9 Flows with combustion wav
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9.2. CONDITIONS THAT MUST BE SATISF
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9.3. NORMAL FLAME FRONT 235 9.3 Nor
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9.4. INCLINED FLAME FRONT 237 60 50
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9.5. ENTROPY JUMP ACROSS THE FLAME
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9.5. ENTROPY JUMP ACROSS THE FLAME
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9.6. VORTICITY ACROSS THE FLAME 243
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Chapter 10 Aerothermodynamic field
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10.1. INTRODUCTION 247 form numeric
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10.1. INTRODUCTION 249 ∆ P /∆ P
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10.2. TSIEN METHOD 251 As aforesaid
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10.2. TSIEN METHOD 253 1.0 λ=6.0 M
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10.3. METHOD OF FABRI-SIESTRUNCK-FO
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10.3. METHOD OF FABRI-SIESTRUNCK-FO
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10.5. CHAMBER WITH SLOWLY VARYING C
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Chapter 11 Similarity in combustion
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11.2. DIMENSIONLESS PARAMETERS OF A
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11.2. DIMENSIONLESS PARAMETERS OF A
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11.3. SCALING OF ROCKETS 267 Furthe
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11.3. SCALING OF ROCKETS 269 From h
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11.4. SCALING OF ROCKETS FOR NON-ST
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11.4. SCALING OF ROCKETS FOR NON-ST
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11.5. FLAME STABILIZATION 275 Flame
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11.5. FLAME STABILIZATION 277 Flame
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11.5. FLAME STABILIZATION 279 which
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Chapter 12 Diffusion flames 12.1 In
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12.1. INTRODUCTION 283 In fact, oth
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Page 310 and 311: 12.3. BOUNDARY CONDITIONS ON THE FL
Page 312 and 313: 12.4. SIMPLIFIED EQUATIONS 293 As f
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Page 320 and 321: Chapter 13 Combustion of liquid fue
Page 322 and 323: 13.2. ATOMIZATION 303 lem has been
Page 324 and 325: 13.4. COMBUSTION 305 solution corre
Page 326 and 327: 13.5. NOTATION 307 2) The phenomeno
Page 328 and 329: 13.6. CONTINUITY EQUATIONS 309 Chem
Page 330 and 331: 13.7. ENERGY EQUATION 311 The value
Page 332 and 333: 13.8. DIFFUSION EQUATIONS 313 13.8
Page 334 and 335: 13.9. COMBUSTION VELOCITY OF THE DR
Page 336 and 337: 13.10. INTEGRATION OF THE EQUATIONS
Page 338 and 339: 13.11. NUMERICAL APPLICATION 319 wh
Page 340 and 341: 13.11. NUMERICAL APPLICATION 321 10
Page 342 and 343: 13.12. COMPARISON WITH EXPERIMENTAL
Page 344 and 345: 13.14. COMBUSTION OF FUEL SPRAYS 32
Page 346 and 347: 13.15. DROPLET EVAPORATION 327 4 0.
Page 348 and 349: 13.15. DROPLET EVAPORATION 329 1 0.
Page 350 and 351: 13.16. APPENDIX: APPLICATION OF PRO
Page 352 and 353: 13.16. APPENDIX: APPLICATION OF PRO
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