[1] Bartlett, E. P. and Kendall, R. M., “Nonsimilar Solution of the Multicomponent Laminar Boundary Layer by an Integral Matrix Method,” NASA CR-1062, Part I, 1967.
[2] Anderson, L. W. and Kendall, R. M., “A Nonsimilar Solution for Multicomponent Reacting Laminar and Turbulent Boundary Layer Flows Including Transverse Curvature,” AFWL TR-69-106, 1970.
[3] Hamilton, H. H., Millman, D. R. and Greendyke, R. B., “Finite-Difference Solution for Laminar or Turbulent Boundary Layer Flow over Axisymmetric Bodies with Ideal Gas, CF4, or Equilibrium Air Chemistry,” NASA CR-3271, 1992.
[4] Catherall, D. and Mangler, K.W., “The Integration of the Two-Dimensional Laminar Boundary-Layer Equations Past the Point of Vanishing Skin Friction,” Journal of Fluid Mechanics, Vol. 26, Issue 01, 1966, pp.163-182.
[5] Lewins, J. D. “Comparative Solutions to the Integral-Approximate Thermal Boundary Layer Equations for a Flat Plate,” International Journal of Mechanical Engineering Education, Vol. 32, Issue 4, 2004, pp. 316-344.
[6] Dejarnette, F. R., Hamilton, A. H., Weilmuenster K. J. and Cheatwood F. M., “A Review of Some Approximate Methods Used in Aerodynamic Heating Analysis,” Journal of Thermo physics, Vol. 1, No. 1 1978, pp. 5-12.
[7] Dejarnette, F. R and Hamilton, H. H., “Inviscid Surface Streamlines and Heat Transfer on Shuttle-Type Configurations,” Journal of Spacecraft, Vol. 10, No. 5 , 1973, pp.314-321.
[8] Riley, C. J. and Dearnette, F. R, “Engineering Aerodynamic Heating Method for Hypersonic Flow,” Journal of Spacecraft and Rockets, Vol. 29, No. 3, 1992, pp.327-339.
[9] Shimshi, J. P. and Walberg, G. D., “Aerodynamic Heating to Spherically Blunted Cones at Angle of Attack,” Journal of Spacecraft and Rockets, Vol. 32, No 33, 1995, pp. 559-561.
[10] Carlson, H. A., “Aerothermodynamics Analyses of Hypersonic Blunt Body Flows,” Journal of Spacecraft and Rocket, Vol. 36, No. 6, 1999, pp. 912-915.
[11]
Zoby, E. V., Moss, J. N. and Sutton, K., “Approximate Convecting Heating Equations for Hypersonic Flows,” Journal of Spacecraft, Vol.18, No.1, 1981, pp 64-70.
[12] Anderson, J. D. Hypersonic and High Temperature Gas Dynamics, NewYork: McGraw-Hill Book Company, 1989.
[13] Eckert, E. R. G., “Engineering Relations for Friction and Heat Transfer to Surfaces in High Velocity Flow,” Journal of the Aeronautical Sciences, Vol. 22, No .8, 1955, pp. 585-587.
[14] Fay, J. A. and Riddle, F. R., “Theory of Stagnation Point Heat Transfer in Dissociated Air,” Journal of the Aerospace Sciences, Vol. 25, No.2, 1958, pp. 73-85.
[15] Kamali Moghadam, R. and Salimi, M. R. “Hypersonic Flow Solution around the Axisymmetric Reentry Vehicles Using Laminar Boundary Layer Equations by Integral Matrix Method,” the first Aero-Hydro Conference, Iran, 2012 (In Persian).
[16] Cleary, J. W., “Effects of Angle of Attack and Bluntness on Laminar Heating- Rate Distributions of Angle 15 Cone at a Mach Number of 10.6,” NASA Technical Note, TN D-5450, October 1969.
[17] Cheatwood, F. and Dejarnet, F. R., “Approximate Viscous Shock Layer Technique for Calculating Hypersonic Flows about Blunt-Nosed Bodies,” Journal of Spacecraft and Rockets, Vol. 31, No. 4, 1994, pp. 621-629.
[18] Anderson, E. C., Lewis, H., “Laminar or Turbulent Boundary-Layer Flows of Perfect Gases or Reacting Gas Mixtures in Chemical Equilibrium,” NASA CR-1893, 1971.
[19] Hollis, B. R. and Perkins J. N., “Comparison of Experimental and Computational Aerothermodynamics of a 70-deg Sphere-Cone”, AIAA 96-1867, 1996.