Rowan-Gollan-PhD-Thesis - Mechanical Engineering - University of ...

More documents

Recommendations

Info

154 References [68] HOSHIKAZI, H., WILSON, K.: 1967. Convective and radiative heat transfer during super- orbital entry. AIAAJournal5(1):25–35 [69] ELBERT, G., CINNELLA, P.: 1993. Axisymmetric radiative heat transfer calculations for flows in chemical non-equilibrium. AIAA Paper 93-0139 [70] OLSTAD, W.: 1971. Nongray radiating flow about smooth symmetric bodies. AIAA Jour- nal9(1):122–130 [71] SAKAI, T., SAWADA, K., PARK, C.: 1997. Assessment of Planck-Rosseland-Gray model for radiating shock layer. AIAA Paper 97-2560 [72] SAKAI, T., SAWADA, K., PARK, C.: 1998. Calculation of radiating flowfield behind a reflected shock wave in air. AIAA Paper 98-0861 [73] SAKAI, T., TSURU, T., SAWADA, K.: 2001. Computation of hypersonic radiating flowfield over a blunt body. JournalofThermophysicsandHeatTransfer15(1):91–98 [74] HARTUNG, L.: 1991. Development of a nonequilibrium radiative heating prediction method for coupled flowfield solutions. AIAA Paper 91-1406 [75] FUJITA, K., ABE, T.: 2003. Development of a radiation analysis code for hypervelocity reentry applications. In: The Insititute of Space and Aeronautical Science, Report SP No. 17, pp. 69–82 [76] PARK, C.: 1985. Nonequilibrium air radiation (NEQUAIR) program: User’s manual. NASA Technical Memorandum 86707, NASA Ames Research Center [77] BOTTIN, B.: 1999. Aerothermodynamic model of an Inductively-Coupled Plasma Wind Tunnel. Docteur en Sciences Appliquées thesis, Université de Liège / Von Karman Institute for Fluid Dynamics [78] ORAN, E., BORIS, J.: 2001. Numerical Simulation of Reactive Flow. Cambridge University Press, New York, USA, 2nd edition [79] HARTUNG, L., MITCHELTREE, R., GNOFFO, P.: 1991. Stagnation point nonequilibrium radiative heating and the influcence of energy exchange models. AIAA Paper 91-0571 [80] BALAKRISHNAN, A., PARK, C., GREEN, M.: 1986. Radiative viscous shock layer analysis of Fire, Apollo, and PAET flight data. In: ThermophysicalAspectsofRe-entryFlows,Progress in AstronauticsandAeronautics, volume 103, pp. 514–540. AIAA, New York [81] SHAH, N.: 1979. The Computation of Radiation Heat Transfer. Ph.D. thesis, Faculty of Engi- neering, University of London [82] KARL, S.: 2001. Simulation of radiative effects in plasma flows. DC report, von Karman Institute for Fluid Dynamics
References 155 [83] HARTUNG, L., MITCHELTREE, R., GNOFFO, P.: 1992. Coupled radiation effects in thermo- chemical nonequilibrium shock-capturing flowfield calculations. AIAA Paper 92-2868 [84] GNOFFO, P. A.: 1989. Upwind-biased point-implicit relaxation strategies for viscous hypersonic flow. AIAA Paper 89-1972 [85] HARTUNG, L., MITCHELTREE, R., GNOFFO, P.: 1994. Coupled radiation effects in thermo- chemical nonequilibrium shock-capturing flowfield calculations. AIAA Journal of Ther- mophysics andHeat Transfer8(2):244–250 [86] SAKAI, T., SAWADA, K.: 2001. Calculation of nonequilibrium radiation from a blunt-body shock layer. JournalofThermophysicsandHeat Transfer15(1):99–105 [87] MATSUYAMA, S., SAKAI, T., SASOH, A., SAWADA, K.: 2003. Parallel computation of fully coupled hypersonic radiating flowfield using multiband model. Journal of Thermophysics and HeatTransfer17(1):21–28 [88] OLEJNICZAK, J., WRIGHT, M., PRABHU, D., TAKASHIMA, N., HOLLIS, B., ZOBY, E. V., SUTTON, K.: 2003. An analysis of the radiative heating environment for aerocapture at Titan. AIAA Paper 2003-4953 [89] WHITING, E., PARK, C., LIU, Y., ARNOLD, J., PATERSON, J.: 1996. NEQAIR96, nonequil- brium and equilibrium radiative transport and spectra program: User’s manual. NASA Reference Publication 1389, NASA [90] WRIGHT, M. J., BOSE, D., OLEJNICZAK, J.: 2005. Impact of flowfield-radiation coupling on aeroheating for Titan aerocapture. Journal of Thermophysics and Heat Transfer 19(1):17– 27 [91] JACOBS, P. A.: 1996. MB CNS: A computer program for the simulation of transient com- pressible flows. Department of Mechanical Engineering Report 10/96, The University of Queensland, Brisbane [92] JACOBS, P. A.: 1991. Single-block Navier-Stokes integrator. ICASE Interim Report 18 [93] JACOBS, P. A.: 1998. MB CNS: A computer program for the simulation of transient com- pressible flows; 1998 Update. Department of Mechanical Engineering Report 7/98, The University of Queensland, Brisbane [94] JACOBS, P. A.: 1992. An approximate Riemann solver for hypervelocity flows. AIAA Journal 30(10):2558–2561 [95] LIOU, M.-S., STEFFEN, Jr., C. J.: 1993. A new flux splitting scheme. JournalofComputational Physics107(1):23–39 [96] WADA, Y., LIOU, M.-S.: 1997. An accurate and robust flux splitting scheme for shock and contact discontinuities. SIAMJournalon ScientificComputing18(3):633–657
Page 1 and 2:
THE UNIVERSITY OF QUEENSLAND The Co
Page 3 and 4:
Statement of Contributions to Joint
Page 5 and 6:
None. Statement of Parts of the The
Page 7 and 8:
Additional Published Works by the A
Page 9 and 10:
Abstract During atmospheric entry,
Page 11 and 12:
Keywords hypersonics, atmospheric-e
Page 13 and 14:
4.2.2 Reaction rate coefficients .
Page 15 and 16:
C.2.5 Jachimowski with the modifica
Page 17 and 18:
5.3 Relaxation time for O2-O V-T ex
Page 19 and 20:
List of Symbols Some symbols which
Page 21:
αν : absorptivity coefficient at
Page 24 and 25:
2 Introduction Chapter 1 building a
Page 26 and 27:
4 Introduction Chapter 1 Figure 1.1
Page 28 and 29:
6 Introduction Chapter 1 Navier-Sto
Page 30 and 31:
8 Introduction Chapter 1 sively by
Page 32 and 33:
10 Introduction Chapter 1 important
Page 35 and 36:
Chapter 2 Background for Aeroshell
Page 37 and 38:
Section 2.1 Physics of atmospheric-
Page 39 and 40:
Section 2.2 Modelling of atmospheri
Page 41 and 42:
Page 43 and 44:
Page 45 and 46:
Page 47 and 48:
Page 49:
Section 2.3 Summary 27 flow. A revi
Page 52 and 53:
30 Flow Solver Chapter 3 For low-or
Page 54 and 55:
32 Flow Solver Chapter 3 substitute
Page 56 and 57:
34 Flow Solver Chapter 3 1.0 0.8 0.
Page 58 and 59:
36 Flow Solver Chapter 3 shock solu
Page 60 and 61:
38 Flow Solver Chapter 3 Table 3.4:
Page 62 and 63:
40 Flow Solver Chapter 3 3.3 Valida
Page 64 and 65:
42 Flow Solver Chapter 3 stream and
Page 66 and 67:
44 Flow Solver Chapter 3 δ/D 0.25
Page 68 and 69:
46 Flow Solver Chapter 3 sation of
Page 71 and 72:
Chapter 4 Chemical Nonequilibrium C
Page 73 and 74:
Section 4.1 A mixture of thermally
Page 75 and 76:
Section 4.1 A mixture of thermally
Page 77 and 78:
Section 4.2 Calculation of chemical
Page 79 and 80:
Section 4.2 Calculation of chemical
Page 81 and 82:
Section 4.3 A mass-conserving formu
Page 83 and 84:
Section 4.4 Verification of the mod
Page 85 and 86:
Page 87 and 88:
Page 89 and 90:
Section 4.5 Validation of the model
Page 91 and 92:
Page 93 and 94:
Page 95 and 96:
Page 97 and 98:
Page 99 and 100:
Section 4.6 The inclusion of diffus
Page 101 and 102:
Section 4.6 The inclusion of diffus
Page 103 and 104:
Section 4.7 Summary 81 mass fractio
Page 105 and 106:
Chapter 5 Vibrational Nonequilibriu
Page 107 and 108:
Section 5.1 A mixture of perfect ga
Page 109 and 110:
Section 5.2 Energy exchange mechani
Page 111 and 112:
Section 5.3 Calculation of vibratio
Page 113 and 114:
Page 115 and 116:
Page 117 and 118:
Section 5.4 Coupling of chemistry a
Page 119 and 120:
Page 121 and 122:
Page 123 and 124:
Page 125 and 126: Section 5.5 Verification of the mod
Page 131 and 132: Section 5.6 Summary 109 temperature
Page 133: Section 5.6 Summary 111 are separab
Page 136 and 137: 114 Applications Chapter 6 In this
Page 138 and 139: 116 Applications Chapter 6 mode, th
Page 140 and 141: 118 Applications Chapter 6 the shoc
Page 142 and 143: 120 Applications Chapter 6 Table 6.
Page 144 and 145: 122 Applications Chapter 6 species
Page 146 and 147: 124 Applications Chapter 6 pressure
Page 148 and 149: 126 Applications Chapter 6 pressure
Page 150 and 151: 128 Applications Chapter 6 To demon
Page 152 and 153: 130 Applications Chapter 6 value of
Page 154 and 155: 132 Applications Chapter 6 Table 6.
Page 156 and 157: 134 Applications Chapter 6 Figure 6
Page 158 and 159: 136 Applications Chapter 6 p, kPa 1
Page 160 and 161: 138 Applications Chapter 6 cone whi
Page 162 and 163: 140 Applications Chapter 6 t = 1.35
Page 164 and 165: 142 Applications Chapter 6 of the m
Page 166 and 167: 144 Conclusion Chapter 7 chemical a
Page 168 and 169: 146 Conclusion Chapter 7 7.1 Contri
Page 171 and 172: References [1] LEBRETON, J.-P., WIT
Page 173 and 174: References 151 Conference CTAC-2003
Page 175: References 153 [53] GLAISTER, P.: 1
Page 179 and 180: References 157 around a cylinder an
Page 181 and 182: References 159 [139] SCHALL, E., BU
Page 183 and 184: References 161 [167] PARK, C.: 1988
Page 185 and 186: Appendix A Input files for Chapter
Page 187 and 188: Appendix A Input files for Chapter
Page 189: Appendix A Input files for Chapter
Page 192 and 193: 170 Analytical solution for an obli
Page 200 and 201: 178 Reaction schemes Appendix C C.1
Page 202 and 203: 180 Reaction schemes Appendix C Rea
Page 204 and 205: 182 Reaction schemes Appendix C Rea
Page 213 and 214: Appendix D Input files for Chapter
Page 215: Appendix D Input files for Chapter
show all

Rowan-Gollan-PhD-Thesis - Mechanical Engineering - University of ...

Create successful ePaper yourself

Delete template?

Save as template?