1 |
Dunlap, R., Blackner, A. M., Waugh, R. C., Brown, R. S. and Willoughby, P. G., 1990, 'Internal Flow Field Studies in a Simulated Cylindircal Port Rocket Chamber,' J. Prop. Power, Vol. 6, No. 6, pp. 690-704
|
2 |
Kasagi, N. and Shikazono, N., 1995, 'Contribution of Direct Numerical Simulation to Understanding and Modeling Turbulent Transport,' Proc. R. Soc. Lond. A., Vol. 45, pp. 257-292
|
3 |
Beddini, R. A., 1986, 'Injection-Induced Flows in Porous Walled Ducts,' AIAA J., Vol. 24, No. 11, pp. 1766-1773
ScienceOn
|
4 |
Lund, T., Wu, X. and Squires, K., 1998, 'Generation of Turbulent Inflow Data for Spatially Developing Boundary Layer Simulation, J. Comput. Physics, Vol. 140, pp. 233-258
DOI
ScienceOn
|
5 |
Harlow, F. H. and Welch, J. E., 1965, 'Numerical Calculation of Time Dependent Viscous Incompressible Flow of Fluid with Free Surface,' Phys. Fluids, Vol. 8, pp. 2182-2189
DOI
|
6 |
Kim, J., Moin, P. and Moser, R., 1989, 'Turbulence Statistics in Fully Developed Channel Flow at Low Reynolds Number,' J. Fluid Mech, Vol. 177, pp. 133-166
DOI
ScienceOn
|
7 |
Liou, T. M. and Lien, W. Y., 1998, 'Numerical Simulations of Injection-Driven Flows in a Two Dimensional Nozzleless Solid Rocket Motor,' J. Prop. Power, vol. 11, No. 4, pp. 600-606
ScienceOn
|
8 |
Miyauchi, T. and Tanahashi, M., 1993, 'Test case : Temporally Developing Chemically Reacting Turbulent Mixing Layer,' http://www.thtlab.t.u-tokyo.ac.jp.
|
9 |
Na, Y., Papavassiliou, D. V. and Hanratty, T., 1999, 'Use of Direct Numerical Simulation to Study the Effect of Prandtl Number on Temperature Fields,' Int. J. Heat and Fluid Flow, Vol. 20, pp. 187-195
DOI
ScienceOn
|
10 |
Spalart, P. R., Moser, R. D. and Rogers, D., 1991, 'Spectral Methods for the Navier-Stokes Equations with One Infinite and Two Periodic Directions,' J. Comput. Phys., vol. 96, pp. 297-324
DOI
ScienceOn
|
11 |
Traineau, J. -C., Hervat, P. and Kuentzmann, P., 'Cold Flow Simulations of a two Dimensional Nozzleless Rocket Motor,' Tech. Rep. 86-1447. AIAA
|
12 |
Williams, F. A., Barrere, M. and Huang, N. C., 1969, 'Fundamental Aspects of Solid Propellant Rockets,' NATO AGARDograph, No. 16
|