[1] Shaw, C., Shan, Y.Y., Qin. N., “Development of a Local MQ-DQ-Based Stencil Adaptive Method and Its Application to Solve Incompressible Navier-Stokes Equations,” International Journal Number Method Fluids, Vol. 55, Issue 4, 2007, pp. 367- 386.
[2] Shaw, C. and Qin, N., “Solution of the Navier-Stokes Equations for the Flow around an Aerofoil in Oscillating Free Stream,” Proceeding of the 20th Congress of the International Council of the Aeronautical Sciences, ICAS, Vol. 1, 1996, pp.19-29.
[3] Lawrence, S. L, Chaussee. D. S. and Tannehill, J. C., “Application of an Upwind Algorithm to the Three-Dimensional Parabolized Navier-Stokes Equations,” AIAA paper 87-1112-CP, June 1987.
]4] Birch, T., Prince. S., Ludlow, D. K. and Qin. N., “The Application of a Parabolized Navier-Stokes Solver to Some Hypersonic Flow Problems”, AIAA 2001-1753, 10th International Space Planes and Hypersonic Systems and Technologies Conference, Kyoto, Japan, 2001.
[5] Esfahanian, V., Hejranfar, K. and Mahmoodi Darian, H., “Implementation of High-Order Compact Finite-Difference Method to Iterative Parabolized Navier-Stokes Equations,” Proceedings of the 25th International Congress of the Aeronautical Sciences, ICAS2006, Hamburg, 2006.
[6] Miner, E. W. and Lewis, C. H., “Hypersonic Ionizing Air Viscous Shock-Layer Flows Over Nonanalytical Blunt Bodies,” NASA CR-2550, 1975.
[7] Thompson, R. A., “Comparison of Nonequilibrium Viscous Shock-layer Solutions with Shuttle Heating Measurements,” Journal of Thermophysics and Heat Transfer, Vol. 4, No. 2, 1990, pp. 162-169.
[8] Noori, S., Ghasemloo, S. and Mani, M., “A New Method for Solution of Viscous Shock Layer Equations,” Journal of Aerospace Engineering, Vol. 224, part G, 2010.
[9] Noori, S., Karimian, S.M.H. and Malekzadehdirin, M., “Numerical Solution of Three-Dimensional Viscous Shock Layer Using Axisymmetric Analog the Streamlines,” International Journal of Numerical Methods for Heat & Fluid Flow, Vol.18, No.1, 2008, pp. 36-49.
[10] Hamilton, H. H., Dejarnette, F.R. and Welmuenstrer, K.J., “Application of Axisymmetric Angle for Calculating Heating in Three-Dimensional Flows,” Journal of Spacecraft and Rockets, Vol. 24, No. 4, 1987, pp. 296-302.
[11] Hamilton. H. H., Greene, F. A. and Dejarnette, F. R., “An Approximate Method for Calculating Heating Rates on Three-Dimensional Vehicles,” AIAA paper 93-2881, 1993.
[12] Dejarnette, F. R. and Hamilton, H. H.,“Aerodynamic Heating on 3-D Bodies Including the Effects of Entropy-Layer Swallowing,” Journal of Spacecraft and Rockets, Vol.12, No.1, 1975, pp. 5-12.
[13] Dejarnette, F. R. and Hamilton, H. H., “Inviscid Surface Streamlines and Heat Transfer on Shuttle-Type Configurations,” Journal of Spacecraft and Rockets, Vol.10, No.5, 1973, pp. 314-321.
[14] Zoby, E. V. and Simmonds, A. L., “Engineering Flow Field Method with Angle-of-Attack Applications”, Journal of Spacecraft and Rockets, Vol. 22, No. 4, 1985, pp. 398-405.
[15] Hamilton, H. H., Greene, F. A. and Dejarnette, F. R., “Approximate Method for Calculating Heating Rates on Three-Dimensional Vehicles,” Journal of Spacecraft and rockets, Vol. 31. No. 3, 1994, pp. 345-354.
[16] Riley, C. J. and Dejarnette, F. R., “Engineering Aerodynamic Heating Method for Hypersonic Flow,” Journal of Spacecraft and Rockets, Vol. 29, No. 3, 1992, pp.327-339.
[17] Maslen, S. H., “Inviscid Hypersonic Flow Past Smoth Symmetric Bodies,” AIAA Journal, Vol. 2, 1964, pp.1055-1061.
[18] Zoby, E.V., Moss, J.J. and Sutton, K., “Approximate Convective-Heating Equations for Hypersonic Flows,” Journal of Spacecraft and Rockets, Vol. 18, No.1, 1981, pp. 64-70.
[19] White, F. M., Viscous Fluid Flow, McGraw-Hill Book Company, New York, USA, 1974.
[20] Dejarnette, F. R.,Hamilton, H. 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.
[21] 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.
[22]Van Dyke, M.D., Milton, D. and Gordon, H. D., “Supersonic Flow Past a Family of Blunt Axisymmetric Bodies,” NASA TR R-1, 1959.
[23] Holt., M. and Hoffman Gilbert, H., “Calculation of Hypersonic Flow Past Sphere and Ellipsoids,” American Rocket Soc., 61-209-1903, 1961.
[24] Mitcheltree, R. A., DiFulvio, M., Horvath, T. J. and Braun, R. D., “Aero Thermal Heating Predictions for Mars Microprobe,” Journal of Spacecraft and Rockets, Vol. 36, No. 3 , pp. 405-411, 1999.
[25] Miller III, C. G., “Measured Pressure Distributions, Aerodynamic Coefficients, and Shock Shapes on Blunt Bodies at Incidence in Hypersonic Air and CF4,” NASA TM-84489, 1982.