REFERENCES
- MacCormack, R.W., A Numerical Method for Solving the Equations of Compressible Viscous Flow, AIAA Journal, vol. 20, no. 9, pp. 1275–1281, 1982.
- Baldwin, B.S., and Lomax, H., Thin Layer Approximation and Algebraic Model for Separated Turbulent Flows, AIAA Paper 78–257, AIAA 16th Aerospace Sciences Meeting, January 1978.
- Serpico, M., Schettino, A., Ciucci, A., Falconi, D., and Fabrizi, M., Base Flow Predictions for a Lightsat Launcher at Supersonic Speeds, Journal of Spacecraft and Rockets, vol. 36, no. 2, pp. 247–254, 1999.
- Tina, T., and Unnikrishnan, C., Base Flow Studies for a Single Engine Launch Vehicle Configuration, Journal of Spacecraft and Rockets, vol. 48, no. 3, pp. 414–419, 2011.
- Bartosiewicz, Y., Mercadier, Y., and Proulx, P., Numerical Investigations on Dynamics & Heat Transfer in a Turbulent Under-Expanded Jet, AIAA Journal, vol. 40, pp. 2257–2265, Nov, 2002.
- Evans, R.L., and Sparks, O.L., Launch Deflector Design Criteria and Their Application to the SATURN C-1 Deflector, NASA TND-1275, 1963.
- Ramanujachari, V., Vijaykant, S., Roy, R.D., and Ghanegaonkar, P.M., Heat Transfer due to Supersonic Flow Impingement on a Vertical Plate, International Journal of Heat and Mass Transfer, vol. 48, no. 17, pp. 3707–3712, 2005.
- Fay, F.A., and Riddell, F.R., Theory of Stagnation Point Heat Transfer in Dissociated Air, Journal of Aeronautical Science, vol. 25, pp. 73–85, 1958.
- Swan, R.T., Pittman, C.M., and Smith, J.C., One Dimensional Numerical Analysis of the Transient Response of Thermal Protection Systems, NASA TN D 2976, 1965.
- Patankar, S.V., A Numerical Method for Conduction in Composite Materials Flow in Irregular Geometries and Conjugate Heat Transfer, Proceedings of Sixth International Heat Transfer Conference, vol. 36, pp. 297–302, Toronto, Canada, 1978.
- Patankar, S.V., Baliga B.R., A New Finite Difference Scheme for Parabolic Differential Equations, Journal of Numerical Heat Transfer, vol. 1, pp. 27–37, 1978.