1 |
Davenas, A., Solid rocket propulsion technology, 1st ed., Pergamon Press, U.K., pp. 1-32, 1992.
|
2 |
Bartz, D.R., "Turbulent Boundary layer and heat transfer from rapidly accelerating flow of rocket combustion gases and of heated air", Advances in Heat Transfer, Vol. 2, pp. 1-108, 1965.
|
3 |
Ellis, R.A., "NASA Space Vehicle Design Criteria (Chemical Propulsion)-Solid Rocket Motor Nozzles," NASA SP-8115, 1975.
|
4 |
Shames, I.H., Mechanics of fluids, 4th ed., McGraw-Hill, N.Y., U.S.A., Ch. 10, 2003.
|
5 |
Levy, D., "Introduction to numerical analysis," Department of Mathematics and Center for Scientific Computation and Mathematical Modeling, University of Maryland, Baltimore, M.D., U.S.A., 2010.
|
6 |
Schlichting, H., Boundary-Layer Theory, 7th ed., McGraw Hill Inc., New York, N.Y., U.S.A., pp. 454, 1979.
|
7 |
Morkovin, M.V., Effects of Compressibility on Turbulent Flows, A. Favre ed., Gordon and Breach Inc., New York, N.Y., U.S.A., pp. 367- 380, 1964.
|
8 |
Bae, J.Y., Lee, Y.J., Bae, H.M., Ham, H.C. and Cho, H.H., "Conjugate simulation of rocket nozzle with 1-D algebraic thermal decomposition equation," 2015 KSPE Fall Conference, Jeju, Korea, pp. 145-148, Nov. 2015.
|
9 |
Kumar, R.R., Vinod, G., Renjith, S., Rajeev, G., Jana, M.K. and Harikrishnan, R., "Thermostructural analysis of composite structures," Materials Science and Engineering: A, Vol. 412, No. 1, pp. 66-70, 2005.
DOI
|
10 |
Lapp, P. and Quesada, B., "Analysis of solid rocket motor nozzle," 28th Joint Propulsion Conference and Exhibit, Nashville, T.N., U.S.A, AIAA 92-3616, Jul. 1992.
|
11 |
Boyarintsev, V.I. and Zvyagin, Yu. V., "Turbulent Boundary Layer on Reacting Graphite Surface," 5th Int. Heat Transfer Conference, Tokyo, Japan, pp. 264-268, Sep. 1974.
|
12 |
Hwang, K.Y., Yim, Y.J., Ham, H.C., Kang, Y.G. and Bae, J.C., "Effects of Solid Propellant Gases on the Thermal Response of Nozzle Liner," Journal of the Korean Society of Propulsion Engineers, Vol. 11, No. 2, pp. 26-36, 2007.
|
13 |
Hwang, K.Y. and Kang, Y.G., "Two-dimensional Thermal Analysis for Carbonacious Thermal Liner of Rocket Nozzle with Ablation and In-depth Pyrolysis," Journal of the Korean Society of Propulsion Engineers, Vol. 3, No. 2, pp. 37-47, 1999.
|
14 |
Kim, Y.C., "Thermal Decomposition and Ablation Analysis of Solid Rocket Propulsion," Journal of the Korean Society of Propulsion Engineers, Vol. 14, No. 5, pp. 32-44, 2010.
|
15 |
McBride, B.J. and Gordon, S., "Computer Program for Calculation of Complex Chemical Equilibrium Composition and Applications, II. Users Manual and Program Description," NASA RP-1311, 1996.
|