references - inflibnetshodhganga.inflibnet.ac.in/bitstream/10603/71691/15/15_references.pdf · ......

12
159 . References 1. Barrere, M., Jaumotte, A., Veubeke, B.F.D. and Vanden1<erckhove, 1., "Elsevier Publishing Company, Amsterdam, 1960, pp56-129. 2. Anon., "Solid Rocket Motor Nozzles", NASA Space Vehicle Design Criteria, NASA SP-8115, June 1975. 3. Bartlet, E.P., "Thermal Protection of Rocket Motor Structures", Aerospace Engineering, Vo1.22, 1963, pp86-89. 4. Beam, RM. and Warming, R.F., "An Implicit Factored Scheme for the Compressible Navier-Stokes Equations", AIAA Journal, VoLl6, No.4, 1978. pp393-402. 5. William, T.H. and Steger, J.L., "linplicit Finite Difference Simulations of Three- Dimensional Compressible Flow", AIAA Journal, VoLl8, No.2, 1980, pp159- 167. 6. Conti, RJ., MacCormack, R.W., Groener, L.S. and Fryer, 1.M., "Practical Navier-Stokes Computation of Axisymmetric Reentry Flow Fields with Coupled Ablation and Shape Change", AlAA Paper 92-0752, 1992. 7. Cline, M.C., "VNAP2: A Computer Program for Computation of Two- Dimensional, Time Dependent, Compressible, Turbulent Flow", Los Alamos National Laboratory, LA-8872, 1981. 8. Shukla, K.N. and Sankara Rao, K., "Heat and Mass Transfer in a Gas Loaded Heat Pipe", ZAMM, Vo1.63, 1981, pp575-580. 9. MacCormack, RW., "A Numerical. Method for Solving the Equations of Compressible Viscous Flow", AlAA Paper 81-0110, Jan. 1981. 10. MacCormack, RW., "Current Status of Numerical Solution of the Navier-Stokes Equations", AIM Paper 85-0032, Jan. 1985. 11. Goldstein, M.E. and Lieb, S.S., "Nonlinear Evolution of Oblique Waves on Compressible Shear Layers", Journal of Fluid Mechanics, Vol.191 , 1988, pp481- 515. 12. Schetz, J.A., Billig, F.S. and Favin, S., "Numerical Solution of Ramjet Nozzle Flows", AIAA Paper 85-1270, July 1985.

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Page 1: References - INFLIBNETshodhganga.inflibnet.ac.in/bitstream/10603/71691/15/15_references.pdf · ... "Numerical Prediction ofFluid Flow and Heat Transfer ... ofa Duct", ASME Journal

159

. References

1. Barrere, M., Jaumotte, A., Veubeke, B.F.D. and Vanden1<erckhove, 1., "ElsevierPublishing Company, Amsterdam, 1960, pp56-129.

2. Anon., "Solid Rocket Motor Nozzles", NASA Space Vehicle Design Criteria,NASA SP-8115, June 1975.

3. Bartlet, E.P., "Thermal Protection of Rocket Motor Structures", AerospaceEngineering, Vo1.22, 1963, pp86-89.

4. Beam, RM. and Warming, R.F., "An Implicit Factored Scheme for theCompressible Navier-Stokes Equations", AIAA Journal, VoLl6, No.4, 1978.pp393-402.

5. William, T.H. and Steger, J.L., "linplicit Finite Difference Simulations of Three­Dimensional Compressible Flow", AIAA Journal, VoLl8, No.2, 1980, pp159­167.

6. Conti, RJ., MacCormack, R.W., Groener, L.S. and Fryer, 1.M., "PracticalNavier-Stokes Computation of Axisymmetric Reentry Flow Fields with CoupledAblation and Shape Change", AlAA Paper 92-0752, 1992.

7. Cline, M.C., "VNAP2: A Computer Program for Computation of Two­Dimensional, Time Dependent, Compressible, Turbulent Flow", Los AlamosNational Laboratory, LA-8872, 1981.

8. Shukla, K.N. and Sankara Rao, K., "Heat and Mass Transfer in a Gas LoadedHeat Pipe", ZAMM, Vo1.63, 1981, pp575-580.

9. MacCormack, RW., "A Numerical. Method for Solving the Equations ofCompressible Viscous Flow", AlAA Paper 81-0110, Jan. 1981.

10. MacCormack, RW., "Current Status ofNumerical Solution of the Navier-StokesEquations", AIM Paper 85-0032, Jan. 1985.

11. Goldstein, M.E. and Lieb, S.S., "Nonlinear Evolution of Oblique Waves onCompressible Shear Layers", Journal of Fluid Mechanics, Vol.191 , 1988, pp481­515.

12. Schetz, J.A., Billig, F.S. and Favin, S., "Numerical Solution of Ramjet NozzleFlows", AIAA Paper 85-1270, July 1985.

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160

13. Wilson, E.A., Adler, D. and Bar-Yoseph, P.Z., "Axisymmetric Thrust VectoringNozzle Performance Prediction", 27th Israel International Conference onMechanical Engineering, Haifa, Israel, May 1998.

14. Wilson, E.A., Adler, D. and Bar-Yoseph, P.Z., "Nozzle PerformanceModelling", AIAA Journal, Vol.40, No.7, July 2002, pp1331-1338.

15. Baldwin, B.S. and Lomax, H., "Thin-Layer Approximation and Algebraic Modelfor Separated Turbulent Flows", AIAA Paper 78-257, Jan. 1978.

16. Van Driest, E.R., "On Turbulent Flow Near a Wall", Journal of AerospaceSciences, Vol.23, 1956, p1007.

17. Klebanoff, P.S., "Characteristics of Turbulence in a Boundary Layer with ZeroPressure Gradient", NACA Report No. 1247, 1955.

18. Cebeci, T., Smith, A.M. and Mosinskis, GJ., "Solution of the IncompressibleTurbulent Boundary Layer Equation with Heat Transfer", Journal of HeatTransfer, Vo1.92, 1970, p499.

19. To, W.M. and Humphery, J.A.c., ''Numerical Simulation of Buoyant, TurbulentFlow-I, Free Convection Along a Heated, Vertical Flat Plate", InternationalJournal of Heat and Mass Transfer, Vol.29, No.4, 1986, pp573-592.

20. Humphery, J.A.C. and To, W.M., ''Numerical Simulation of Buoyant, TurbulentFlow-II, Free and Mixed Convection in a Heated Cavity", International Journalof Heat and Mass Transfer, Vol.29, No.4, 1986, pp593-610.

21. Correa, S.M. and Shuy, W., "Computational Models and Methods forContinuous Turbulent Combustion", Progress in Energy and CombustionScience, VoLl3, No.4, 1987, pp249-292.

22. Gottlieb, D. and Orszag, S.A., "Numerical Analysis of Spectral Methods: Theoryand Applications", Society for Industrial and Applied Mathematics,Philadelphia, 1977.

23. Canuto, c., Hussaini, M.Y., Quarteroni, A. and Zang, T.A., "Spectral Methodsin Fluid Dynamics", Springer-Verlag, New York, 1988.

24. Pratt, D.T., "Calculation of Chemically Reacting Flows with ComplexChemistry", Studies in Convection, Edited by B.E.Launder, Vol.2, AcademicPress, New York, 1977.

25. Wilson, G.J., "Computation of Steady and Unsteady Shock Induced CombustionOver Blunt Bodies", Ph.D. Dissertation, Stanford University, Stanford, CD,Dec.1991.

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161

26. Shuen, J.S. and Yoon, S., "Numerical Study of Chemically Reacting FlowsUsing an LU Scheme", AIAA 26th Aerospace Sciences Meeting, AlAA Paper88-0436, NV, Jan. 1988.

27. Park, C., "Injection Induced Turbulence in Stagnation-Point Boundary Layers",AIAA Journal, Vo1.22, No.2, 1984, pp219-225.

28. Ruffin, S.M., Venkatapathy, E., Keener, E.R. and Naaraj, N., "ConventionalDesign Aspects of a NASP Nozzle/After Body Experiment", AlAA Paper 89­0446, Jan. 1989.

29. Shukla, K.N. and Ghosh, D., "ADI Method for Heat Conduction Problems in anOrthogonal Coordinate System", Heat Transfer Engineering, VoLl5, No.2,1994, pp64-72.

30. Baysal, 0., Englewood, W.C., Elesaky, M.E. and Pittmann, J.L., "AdaptiveComputation of Viscous Scramjet After-Body Flows with and withoutMuItispecies", AIAA Paper 89-0009, Jan. 1989.

31. Lal, M. and Nelson, E., "Comparison of 3-D Computation and Experiment forNon-Axisymmetric Nozzles", AIAA Paper 89-0007, Jan. 1989.

32. Beam, R.M. and Warming, R.F., "An Explicit Factored Scheme for theCompressible Navier-Stokes Equations", AlAA Journal, Vo1.16, No.4, 1979,pp303-402.

33. Povinelli, L.A. and Anderson, B.H., "Investigation of Mixing in a TurbofanExhaust Duct, Part-II, Computer Code Application and Verification", AIAAJournal, Vo1.22, No.4, 1984, pp518-525.

34. Povinelli, L.A. and Ehlers, R.C., "Swirling Base Injection for SupersonicCombustion Ramjets", AIAA Journal, Vo1.10, No.9, 1972, ppI243-1244.

35. Balsa, T.F. and Goldstein, M.E., "On the Instabilities of Supersonic MixingLayers: A High Nonlinear Asymptotic Theory", Journal of Fluid Mechanics,Vo1.216, 1990, pp585-612.

36. Hu, J. and Rizzi, A., "Turbulent Flows in Supersonic and Hypersonic Nozzles",AlAA Journal, Vo1.33, No.9, 1995, pp1634-1640.

37. Chen, c.L., Chakravarthy, S.R. and Hung, C.M., "Numerical Investigation ofSeparated Nozzle Flows", AlAA Journal, Vo1.32, No.9, 1994, ppI836-1843.

38. Price, F.C., et. al., "Internal Environment of Solid Rocket Nozzles", AFRPL­TDR-64-140, Philco-Ford .Corporation, July 1964.

Page 4: References - INFLIBNETshodhganga.inflibnet.ac.in/bitstream/10603/71691/15/15_references.pdf · ... "Numerical Prediction ofFluid Flow and Heat Transfer ... ofa Duct", ASME Journal

162

39. Adam, J.M., "On the Determination of Spectral Emissivity in an Optically ThickParticle Cloud", Journal of Quantitative Spectroscopy and Radiation Transfer,Vol.8, No.2, Jan.-Apri11968, pp631-639.

40. Colueci, S.E., et. al., "Experimental Determination of Nozzle Heat TransferCoefficient with Aluminized Propellants", Paper Presented at Solid PropellantRocket Conference, American Rocket Society, Salt Lake City, UT, Feb.1961.

41. Watson, G.H. and Lee, A.L., "Solid Rocket Booster Thermal Radiation Model",NASA CR-144300, Mar. 1976.

42. Boraas, S., "Modeling Slag Deposition in the Space Shuttle Rocket Motor",Journal of Spacecraft and Rockets, Vol.21, No.1, 1984, pp47-54.

43. Peterson, D.L. and Nicolet, W.E., "Heat Shielding for Venus Entry Probes",Journal of Spacecraft and Rockets, VoLll, No.6, 1974, pp382-387.

44. Hwang, C.J. and Chang, G.C., ''Numerical Study of Gas-Particle Flow in a SolidRocket Nozzle", AIAA Journal, Vol.26, No.6, 1988, pp682-689.

45. Anon., "Solid Rocket Motor Nozzles", NASA Space Vehicle Design Criteria,NASA SP-8115, June 1975.

46. Travis, L.P., Fairall, R.S. and Lorene, S.A., "Performance of Solid RocketMotors with Gas Particle Flow", ASME Paper No. 63-AHGT-99, Los Angeles,CA, Mar. 1963. \

47. Elliott, D.G., Bartz, D.R. and Silver, S., "Calculation of Turbulent BoundaryLayer Growth and Heat Transfer in Axisymmetric Nozzles", Technical ReportNo.32-387, Jet Propulsion Laboratory, California, Feb. 1963.

48. Anon., " Aerotherrn Real Gas Energy Integral Boundary Layer Program(ARGEIBL)", User's Manual, Report No. 69-UM-6911, Aerotherm Corporation,Nov. 1969.

49. Bartz, D.R., "A Simple Equation for Rapid Estimation of Rocket NozzleConvective Heat Transfer Coefficients", Jet Propulsion, Jan. 1957, pp49-51.

50. Boldman, D.R., Schmidt, J.F. and Eblers, R.C., "Prediction of Local andIntegrated Heat Transfer in Nozzles Using an Integral Turbulent Boundary LayerMethod", NASA TND-6595, Mar. 1972.

51. Gregg, T., "PNS Simulation of Rocket Nozzle Exhaust Flows", AIAA Paper 88-3345, AIAAlASME/SAE/ASEE 24th Joint Propulsion Conference,Massachusetts, July 1988..

Page 5: References - INFLIBNETshodhganga.inflibnet.ac.in/bitstream/10603/71691/15/15_references.pdf · ... "Numerical Prediction ofFluid Flow and Heat Transfer ... ofa Duct", ASME Journal

163

52. Coles, D.E. and Hirst, E.A., "Computation of Turbulent Boundary Layers",AFOSR-IFP-Stanford Conference, Vol.2-Compiled Data, ThermalsciencesSciences Division, Dept. of Mechanical Engineering, Stanford University, 1969.

53. Wright, C.H. and Lund, R.K., "Internal Aerodynamics of Solid Rocket Motors",Paper Presented at the AIChE Meeting, Salt Lake City, UT, May 1967.

54. Anon., "Aerothenn Charring Material Thermal Response and AblationProgram", User's Manual, Version-3, AFRPL-TR-70-92, Vol.-I, AerothermCorporation, Apr. 1970.

55. Anon., "Aerothenn Axisymmetric Transient Heating and Material AblationComputer Program (ASTHMA-3)", User's Manual, AFRPL-TR-72-24,Aerotherrn Corporation, Jan. 1972.

56. Ellison, J.R., Schoner, RJ. and Thrasher, DJ., "Test Firing of a Castable CarbonRocket Nozzles", AFRPL-TR-69-39, Air Force Rocket Propulsion Laboratory,Feb. 1969.

57. Freidman, H.A., "Effect of Rocket Engine Combustion on Chamber Materials,Part-II, 2-D Computer Program", NAA-RR-6050-2, Rocketdyne Division, NorthAmerican Aviation, Inc., Sep. 1965.

58. Chen, Y.K., Henline, W.D. and Tauber, M.E., "Mars Pathfinder TrajectoryBased Heating and Ablation Calculations", Journal of Spacecraft and Rockets,Vol. 32, No.2, 1995, pp225-230. \

59. Olynick, D.R., Chen, Y.K. and Tuber, M.E., "Forebody TPS Sizing withRadiation and Ablation for the Stardust Sample Return Capsule", AIAA Paper97-2474, June 1997.

60. Chen, Y.K. and Milos, F.S., "Fully Implicit Ablation and Thermal AnalysisProgram (FlAT)", ICCE/4, Fourth International Conference on CompositesEngineering, Edited by D.Hui, University of New Orleans, LA, 1997,pp661,662.

61. Chen, Y.K. and Milos, F.S., "Ablation and Thermal Response Program forSpacecraft Heatshield Analysis", Journal of Spacecraft and Rockets, Vo1.36,No.3, May-June 1999, pp475-483.

62. Pike, R.W., April, G.C. and Valle, E.G.D., "Non-Equilibrium Flow and theKinetics of Chemical Reactions in the Char Zone", NASA CR-66455, July 1967.

Page 6: References - INFLIBNETshodhganga.inflibnet.ac.in/bitstream/10603/71691/15/15_references.pdf · ... "Numerical Prediction ofFluid Flow and Heat Transfer ... ofa Duct", ASME Journal

164

63. April, G.C., Valle, E.G.D. and Pike, R.W., "Transport Phenomena in the CharZone-I, Evaluation of the Energy Transfer for Frozen and Equilibrium Flows",Paper No.1, Third National Meeting of the AIChE, Salt Lake City, May 1967.

64. April, G.C., Pike, R.W. and Valle, E.G.D., "Experimental Verification of theNon-Equilibrium Model for Predicting Behavior in the Char Zone of a CharringAblator", NASA CR-66646, July 1968.

65. Schaefer, J.W. and Dahm, T.1., "Studies of Nozzle Ablative MaterialPerformance for Large Solid Boosters", NASA CR-72080, Dec.1966.

66. Rindal, R.A., Clark, K.1., Moyer, C.B. and Flood, D.T., "Experimental andTheoretical Analysis of Ablative Material Response in a Liquid PropellantRocket Motor", NASA CR-72301, Sep.l967.

67. Arai, N., Tani, T. and Sato, K., "Transient Ablation of Blunt Bodies at Angles ofAttack", Journal of Spacecraft and Rockets, Vo1.21 , No.3, 1984, pp241-245.

68. Molvik, G.A., Milos, F.S., Chen, Y.K. and Squire, T.H., "Computation of HighSpeed Flow Fields with Multi-Dimensional Heat Conduction", AIAA Paper 95­2116, June 1995.

69. Olynick, D.R. and Heline, W.D., "Navier-Stokes Heating Calculation for BenchMark Thermal Protection System Sizing", Journal of Spacecraft and Rockets,Vol.33, No.6, 1996, pp807-814.

70. Yamamoto, Y. and Yoshioka, M., "GFD and FEM Coupling Analysis of OrexAerothermodynamic Flight Data, AIAA Paper 9?-2087, June 1995.

71. Li, H. and Kessab, A.1., "A Coupled FVMlBEM Approach to Conjugate HeatTransfer in Turbine Blades", AIAA Paper 94-1981, June 1994.

72. Li, H. and Kessab, A.J., "Numerical Prediction of Fluid Flow and Heat Transferin Turbine Blades with Internal Cooling", AIAA Paper 94-2933, June 1994.

73. Milos, F.S. and Rasky, D.1., "Review of Numerical Procedures forComputational Surface Thermochemistry", Journal of Thermophysics and HeatTransfer, Vo1.8, No.1, 1996, pp24-34.

74. Luikov, A.V., "Conjugate Convective Heat Transfer Problems", InternationalJournal of Heat and Mass Transfer, VoLl7, 1974, pp257-265.

75. Sucec, J., "Exact Solution for Unsteady Conjugate Heat Transfer in the ThermalEntrance Region of a Duct", ASME Journal of Heat and Mass Transfer, VoLl09,May 1987, pp295-299.

Page 7: References - INFLIBNETshodhganga.inflibnet.ac.in/bitstream/10603/71691/15/15_references.pdf · ... "Numerical Prediction ofFluid Flow and Heat Transfer ... ofa Duct", ASME Journal

165

76. Shope, F.L., "Conjugate Conduction-Convection Heat Transfer with a High­Speed Boundary Layer", AIAA Journal of Thermophysics and Heat Transfer,Vol.8, No.2, Apr.-June 1994, pp275-281.

77. Patanker, S.V. and Spalding, D.B., "A Finite-Difference Procedure for Solvingthe Equations of the Two-Dimensional Boundary Layer", International Journalof Heat and Mass Transfer, VoLlO, No.1 9, 1967, pp1389-1411.

78. Kuo, J.C. and Lin, T.F., "Steady Conjugate Heat Transfer in Fully DevelopedLaminar Pipe Flows", Journal of Thermophysics and Heat Transfer, Vol.2, No.3,1988,pp281-283.

79. Lan, S.c., ang, L.E. and Han, J.C., "Conjugate Heat Transfer in Channels withInternal Longitudinal Fins", Journal of Thermophysics and Heat Transfer, VolJ,No.3, 1989, pp303-308.

80-, Henline, W.D., Palmer, G.E., Milos, F.S., OIYnick, D.R. and Chen, Y.K.,"Aerotherrnodynamic Heating Analysis and Heat Shield Design of an SSTORocket Vehicle for Access-to-Space", AIAA Paper 95-2079, 30th AIAATherrnophysics Conference, San Diego, CA, June 1995.

81. Lin, W.L., Carlson, K.D. and Chen, CJ., ''Numerical Modeling of ConjugateHeat Transfer on Complex Geometries with Diagonal Cartesian Method, Part-I:Methods", ASME Journal of Heat Transfer, VoU21, May 1999, pp253-260.

82. Carlson, K.D., Lin, W.L. and Chen, CJ., ''Numerical Modeling of ConjugateHeat Transfer on Complex Geometries with Diagonal Cartesian Method, Part-II:Applications", ASME Journal of Heat Transfer, VoU21, May 1999, pp261-267.

83. Engelke, W.T., Pyron, C.M.Jr. and Pears, C.D., "Thermal and MechanicalProperties of a Nondegraded and Thermally Degraded Phenolic-CarbonComposites", NASA CR-896, Oct. 1967.

84. Peterson, D.A., Winter, J.M. and Shinn, A.MJr., "Rocket Engine Evaluation ofErosion and Char as Functions of Fabric Orientation for Silica-ReinforcedNozzle Materials", NASA TMX-1721, Jan. 1969.

85. Anon., "Testing of Ablative Specimens at Elevated Temperatures", Final ReportNo. EMTL-1059, FMI-EMTL-W/A No. 5751, Energy Material TestingLaboratory, Biddeford, ME-04005, Jan, 1986.

86. Holzknecht, 8., "An Analytical Model of the Transient Ablation of Polytetra­fluoroethylene Layers", International Journal of Heat and Mass Transfer, Vol.20,1977, pp661-668.

87. Shields, S., "Scout Nozzle Data", NASA CR-145136, Dec. 1976.

Page 8: References - INFLIBNETshodhganga.inflibnet.ac.in/bitstream/10603/71691/15/15_references.pdf · ... "Numerical Prediction ofFluid Flow and Heat Transfer ... ofa Duct", ASME Journal

166

88. Brumenthal, J.L., Larsan, R.D. and Nordberg, R.C., "Determination ofThermophysical Properties of Ablative Materials", NASA CR-65486, July 1966.

89. Brooks, W.A.Jr., "Evaluation of Materials in Entry Heating Simulation", NASATMX-54976, Aug. 1964.

90. Nelson, J.B., "Determination of Kinetic Parameters of Six Ablative Polymers byThermogravimetric Analysis", NASA TND-3919, Apr. 1967.

91. Anderson, J.D.Jr., "Fundamentals of Aerodynamics", McGraw-Hill, Inc.,Singapore, 1991, pp579-589.

92. Serra, R.A., "Determination of Internal Gas Flows by a Transient NumericalTechnique", AIAA Journal, VoLlO, No.5, May 1972, pp603-611.

93. Cline, M.C., "The Computation of Steady Nozzle Flow by a Time DependentMethod", NASA TMX-71918, April1974.

94. Cline, M.e., "NAP: A Computer Program for the Computation of Two­Dimensional Time-Dependent Inviscid Nozzle Flow", LA-5984, Jan. 1977.

95. Chakravarthy, S.R., "Inviscid Analysis of Duel-Thrust Nozzle Flows", AIAAPaper 81-1202, AIAA 14th Fluid and Plasma Dynamics Conference, 23-25 June,1981.

96. Jones, V., and Shukla, K.N., ''Nozzle Flow Simulation", VSSC:TR:215:91,Vikram Sarabhai Space Centre, Trivandrum, India, July 1991.

97. Cline, M.C., "VNAP: A Computer Program for Computation of Two­Dimensional Time-Dependent Compressible Viscous Internal Flow", LA-7326,Nov. 1978.

98. Swanson, R.C., "Navier-Stokes Solution for Non-Axisymmetric Nozzle Flows",AIAA Paper 81-1217, AIAA 14th Fluid and Plasma Dynamics Conference, PaloAlto, California, June 1981.

99. Hasen, G.A., "Navier-Stokes Solution for an Axisymmetric Nozzle", AIAAJournal, Vol. 20, No.9, Sep. 1982, ppI219-1227.

100. Mani, M., Tiwari, S.N., and Drummond, lP.,"Numerical Solution of ChemicallyReacting and Radiating Flows", AIAA Paper 87-0324, AlAA 25 th AerospaceSciences Meeting, Reno, Nevada, Jan. 1987.

Page 9: References - INFLIBNETshodhganga.inflibnet.ac.in/bitstream/10603/71691/15/15_references.pdf · ... "Numerical Prediction ofFluid Flow and Heat Transfer ... ofa Duct", ASME Journal

167

101.Barber, T.J. and Cox Jr., G.B., "Hypersonic Vehicle Propulsion : AComputational Fluid Dynamics Application Case Study", lPropulsion, V.5,NoA, July-Aug. 1989, pp492-501.

102.Smith, RE. and Weigel, B.L., "Analytic and Approximate Boundary FittedCoordinate Systems for Fluid Flow Simulation", AIAA Paper 80-0192, AIAA18th Aerospace Sciences Meeting, Pasadena, California, Jan. 1980.

103.Tulapurkara, E.G., "Turbulence Models For The Computation of Flow PastAirplanes", Prog. Aerospace Sciences, Vol.33, pp71-165, 1997.

I04.MacCormack, RW., "The Effect of Viscosity in Hypervelocity ImpactCratering", AIAA Paper 69-354, AIAA Hypervelocity Impact Conference,Cincinnati, Ohio, Apr. 1969.

105.Shapiro, A.H., "The Dynamics and Thermodynamics of Compressible FluidFlow", Vols.l & 2, The RQnald Press Company, New York, 1953.

106.Zucrow, M.J. and Hoffinann, J.D., "Gas Dynamics",Vol. I, John Wiley and Sons,New York, 1976, pp580-621.

107.Moretti, G. and Abbett, M., "A Time-Dependent Computational Method forBlunt Body Flows", AIAA Journal, VolA, No.12, Dec. 1966, pp2136-2141.

108.Cuffel, RF., Beck, L.H. and Massier, P.F., "Transonic Flow Field in aSupersonic Nozzle with Small Throat Radius of Curvature", AIAA Journal,Vol.7, No.7, July 1969, pp1364-1366. "

109.Mason, M.L., Putnam, L.E. and Richard, J.R., "The Effect of Throat Contouringon Two-dimensional Converging-Diverging Nozzles at Static Conditions",NASA TP-1704, Aug. 1980.

110.Swann, R.T. and Pittman, e.M., ''Numerical Analysis of the Transient Responseof Advanced Thermal Protection System for Atmospheric Entry", NASA TN D­1370, July 1962.

II 1.Swann, RT., Pittman, C.M. and Smith, J.e., "One-Dimensional NumericalAnalysis of the Transient Response of Thermal Protection Systems", NASA TN0-2976, Sep. 1965.

112.Khurana, G.S. and Jones, V., "A Simplified Method of Analysis of CharringMaterials", VSSC:TR:34105:78, June 1978.

113.Curry, D.M., "An Analysis of a Charring Ablation Thermal Protection System",NASA TN D-3150, Nov. 1965.

Page 10: References - INFLIBNETshodhganga.inflibnet.ac.in/bitstream/10603/71691/15/15_references.pdf · ... "Numerical Prediction ofFluid Flow and Heat Transfer ... ofa Duct", ASME Journal

168

I14.Cai, T. and Hou, x., "Simple Method for Numerical Simulation of TemperatureResponse of the Solid Rocket Nozzle", J.Thermophysics and Heat Transfer, Vol­4, No.1, Jan. 1990, pp42-46.

I15.Howe, J.T. and Yang, L., "Earth Atmosphere Entry Thermal Protection byRadiation Black-scattering Ablation Materials", J.Thermophysics and HeatTransfer, Vol.7, No.1, Jan.-Mar. 1993, pp74-81.

I16.Rindal, R.A., Flood, D.T. and Kendall, K.M., "Analytical and ExperimentalStudy of Ablation Material for Rocket Engine Application", NASA CR-54757,Aug. 1965.

117.Taylor, A.G., "A Transient Reaction Kinetics Analysis of Ablation ThroughAerodynamic Heating", General Dynamics Corporation, GDC-ERR-AN-1029,Dec. 1966. .

1I8.Moyer, C.B. and Rindal, R.A., "An Analysis of the Coupled ChemicallyReacting Boundary Layer and Charring Ablator Part-II Finite Difference Solutionfor the In-depth Response of Charring Materials Considering Surface Chemicaland Energy Balances", NASA CR-1061, June 1968.

1I9.Quan, V. "Quasi-Steady Solution for Ablation-Erosion Heat Transfer",J.Spacecraft and Rockets, Vol.7, No.3, Mar. 1970, pp355-357.

120.Jones, V., "In-depth Response of Charring Ablators to High TemperatureEnvironments", Technical Report No. HTCR/195(8)/87, HTCR Division, VikramSarabhai Space Centre, Trivandrum-695022, India, Aug. 1987.

121.Kendall, R.M., Rindall, R.A. and Bartlett, E.P., "A Multi-component BoundaryLayer Chemically Coupled to an Ablating Surface", AIAA -1., Vol.5, No.6, June1967, ppl063-1071.

122.Nelson H. Kemp, "Surface Reaction Rate of an Ablating Polymer", AIAA-J.,Vo1.6, No.9, Sep. 1968, ppI790-1791.

123.Bishop, W.M. and Dicristina, V., "A Prediction Technique for ablative MaterialPerformance Under High Shear Re-entry Conditions", AIAA-1., Vol.6, No.1, Jan.1968, pp59-63.

124.Rornie, F.E., "Carbon-Silica Reaction in Silica-Phenolic Composites", AIAA-1.,Vol.5, No.8, Aug. 1967, ppI511-1513.

125.Hsieh, c.L. and Seader, J.D., "Surface Ablation of Silica-ReinforcedComposites", AIAA-J., VoLll, No.8, Aug. 1973, ppI181-1187.

Page 11: References - INFLIBNETshodhganga.inflibnet.ac.in/bitstream/10603/71691/15/15_references.pdf · ... "Numerical Prediction ofFluid Flow and Heat Transfer ... ofa Duct", ASME Journal

169

126.Seala, S.M. and Ghilbert, L.M. "Sublimation of Graphite at Hypersonic Speeds",AIAA-J., Vol.3, No.9, Sep. 1965, pp1635-1644.

127.Baron, J.R. and Bernstein, H., "Heterogeneous Rate Coupling for GraphiteOxidation", AIAA-J., Vol.9, No.8, Aug. 1971, pp1588-1595.

128.Mathieu, R.D., "Mechanical Spallation of Charring Ablators in HyperthermalEnvironments", AIAA-J., Vol.2, No.9, Sep. 1964, pp1621-1627.

129.Schneider, P.J., Dolton, T.A. and Reed, G.W., "Mechanical Erosion of CharringAblators in Ground Test and Re-entry Environments", AIAA-J., Vol.6, No.1,Jan. 1968,pp64-72.

130.Bishop, W.M. and Minkowyez, W.J. "Decomposition Rate of a Phenolic Resin",AIAA-J., Vol.11, No.4, Apr. 1973, pp438-443.

131.Camahan, B., Luther, H.A. and Wilkes, J.O., "Applied Numerical Methods",John Wiley & Sons, Inc., 1969.

132.Rosenberg, D.D.V., "Methods for the Numerical Solution of Partial DifferentialEquations", American Elsevier Publishing Company, Inc., New York, 1969.

133.Schaefer, J.W., et. al., "Studies of Ablative Material Performance for SolidRocket Nozzle Applications", NASA CR-72429, Mar. 1968.

134.Subramanya, B. and Ramaswamy, K.R., "Performance Evaluation Report ofPSI-0l Nozzle", Report No. ABSD/75'/90, Vikram Sarabhai Space Centre, India,Oct. 1990.

135.Venkatachalapathy, L. and Ramaswamy, K.R., "Performance Evaluation Reportof PSI-02 Nozzle", Report No. ABSD/29/92, Vikram Sarabhai Space Centre,India, Feb. 1992.

136.Nagappa, R., "Development of Large Solid Propulsion Systems for LaunchVehicles", 'Propellants, Explosives, Rockets and Guns', Proceedings of theSecond International High Energy Materials Conference and Exhibit, Dec. 8-10,1998, ITT Madras, India, pp33-39.

137.Paul, J., et. aI., "PS3-HPM-02 Static Test - Report of the Post Test Analysis TaskTeam for Thermal Design Validation", Report No. SMG/SMDD/06/2002, SolidMotors Development Division, Vikram Sarabhai Space Centre, Trivandrum­695022, India, Jan. 2002.

138.Easwaran, V., et. al., "Report on the Post Test Analysis of PS3-08 Nozzle",Report No. SMP/12/93, Solid Motors Project, Vikram Sarabhai Space Centre,Trivandrum-695022, India, Mar. 1993.

Page 12: References - INFLIBNETshodhganga.inflibnet.ac.in/bitstream/10603/71691/15/15_references.pdf · ... "Numerical Prediction ofFluid Flow and Heat Transfer ... ofa Duct", ASME Journal

170

139.Retnam, J.Y., "Post Test Observation Report of AS4 Sea-Level Nozzles", ReportNo. VSSC/SMP/27/93, Solid Motors Project, Vikram Sarabhai Space Centre,Trivandrum-695022, India, June 1983.

140.Achari, S.M, Kutty, M.C.G. and Rajarnohan, A., "Post Test Analysis of SLYNozzles", Report No. PSS/79/TE/03, Solid Propulsion Division, VikrarnSarabhai Space Centre, Trivandrurn-695022, India, Feb. 1987.

141.Jones, V. and Shukla, K.N., "Fluid Flow in Rocket Nozzles", AIAA Paper 98­3840, 34th AIAAlASME/SAE/ASEE Joint Propulsion Conference & Exhibit,Cleveland, Ohio, July 1998.

142.Jones, V. and Shukla, K.N., "In-Depth Response of Charring Ablators to HighTemperature Environments", AIAA Paper No. 99-3462, 33 rd ThermophysicsConference, Norfolk, Virginia, June 1999.

143.Jones, V. and Shukla, K.N., "Performance Analysis of Thermal ProtectionSystem of a Solid Rocket Nozzle", AIAA Paper No. 2002-4196, 38th

AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, July 2002.

144.Swaminathan, R., and Balu, R., "Computation of Nozzle Heat Transfer UsingBoundary-Layer Method", Proceedings of the Technical Sessions, 48th AGM,Aeronautical Society of India, Trivandrum, Jan. 1997.

145.Bartz,. D.R., "Turbulent Boundary-Layer Heat Transfer from RapidlyAccelerating Flow of Rocket Combustion Gases and of Heated Air", Advances inHeat Transfer, Vol.2, Academic Press, 1965.

146.Anon., "SAE Aerospace Applied Thermodynamics Manual", Society ofAutomotive Engineers, Inc., New York, 1969.

147.Roberts, L., "Mass Transfer Cooling Near the Stagnation Point", NACA TN­4391, Sep. 1958.

148.Lemoine, L., "Solid Rocket Nozzle Therrnostructural Behavior", AIAA PaperNo. 75-1339, AIAAlSAE 11 th Propulsion Conference, California, Sep. 1975.

149.Krishnamoorthy, P.A., Aravindakshan Pillai, L., Padmanabhan, M.S. and Pillai,B.C., "Subscale Performance Simulation Testing for High Altitude SolidMotors", ISTS 98-a-I-13, 21 st International Symposium on Space Technologyand Science, Sonic City, Omiya, Japan, May 1998.