1 |
Forsythe J. R., Hoffmann K. A., and Suzen, Y. B., "Investigation of Modified Menter's Two-Equation Turbulence Models for Supersonic Applications", 37th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, AIAA 99-0873, 1999.
|
2 |
Shirazi, S. A., and Truman, C. R., "Simple Turbulence Models for Supersonic and Hypersonic Flows: Bodies at Incidence and Compression Corners", 27th AIAA Aerospace Sciences Meeting, Reno, NV, AIAA 89-0669, 1989.
|
3 |
De Feo, D. M., and Shaw, S. T., "Turbulence Modeling and Supersonic Base Flow", 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, AIAA 2007-1083, 2007.
|
4 |
Chuang, C. C., and Chieng, C. C., "The Computations of Shock-Induced Separated Flows By The k-epsilon Model with Compressibility Modifications", 35th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, AIAA 97-0067, 1997.
|
5 |
Matsuo, K., Miyazato, Y., and Kim, H. D., "Shock Train and Pseudo-Shock Phenomena in Internal Gas Flows", Progress in Aerospace Sciences, Vol. 35, No. 1, 1999, pp. 33-100.
DOI
ScienceOn
|
6 |
Sarkar, S., Erlebacher, B., Hussaini, M., and Kreiss, H., "The Analysis and Modeling of Dilatational Terms in compressible Turbulence", Journal of Fluid Mechanics, Vol. 227, 1991, pp. 473-493.
DOI
|
7 |
Sarkar, S., "Modeling the Pressure-Dilatation Correlation", IC-ASE, Rept. 91-42, Hampton, VA, 1991.
|
8 |
Dash, S., and Kenzakowski, D. C., "A Compressible-Dissipation Extension of the k-epsilon Turbulence Model and Building-Block Data for its Validation", AIAA SDIO Annual Interceptor Technology Conference, Huntsville, AL, AIAA 92-2766, 1992.
|
9 |
Wilcox, D. C., Turbulence Modeling for CFD, Second Ed., DCW Industries, La Canada, California, 2002.
|
10 |
Kim, K. H., Kim, C. A., and Rho, O. H., "Methods for the Accurate Computations of Hypersonic Flows: I. AUSMPW+Scheme", Journal of Computational Physics, Vol. 174, 2001, pp. 38-80.
DOI
ScienceOn
|
11 |
Inger, G. R., and Gendt, C., "An Experimental Study of Transonic Shock/Turbulent Boundary Layer Interaction on a Roughened Surface", 35th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, AIAA 97-0065, 1997.
|
12 |
Mendonca, J., and Sharif, M. A. R, "Performance of Turbulence Models in the Computation of Transonic Flow over a Circular Arc Bump", 35th AIAA Fluid Dynamics Conference and Exhibit, Toronto, Ontario Canada, AIAA 2005-4637, 2005.
|
13 |
Borgar, T. J., "Structure of Self-Excited Oscillations in Transonic Diffuser Flows", AIAA Journal, Vol. 24, No. 1, 1986, pp. 54-61.
DOI
ScienceOn
|
14 |
Chen, C. P., Sajben, M. and Kroutil, J. C., "Shock-Wave Oscillations in a Transonic Diffuser Flow", AIAA Journal, Vol. 17, No. 10, 1979, pp. 1076-1083.
DOI
ScienceOn
|
15 |
Park, J. H., Lee, T. S. and Kim, Y. G., "A Study of Supersonic Jets Impinging on Axisymmetric Cone", Journal of the Korean Society for Aeronautical and Space Science, Vol. 31, No. 7, 2003, pp. 26-31.
|
16 |
Yeom, H. W., Yoon, S. K., and Sung, H. G., "Flow Dynamics at the Minimum Starting Condition of a Supersonic Diffuser to Simulate a Rocket's High Altitude Performance on the Ground", Journal of Mechanical Science and Technology, Vol. 23, Issue 1, 2009, pp. 254-261.
DOI
ScienceOn
|
17 |
Menter, F. R., "Two-Equation Eddy-Viscosity Turbulence Models for Engineering Application", AIAA Journal, Vol. 32, No. 8, 1993, pp. 1598-1605.
|
18 |
Sung, H. G., Yeom, H. W., Yoon, S. K., Kim S. J., and Kim, J. G., "Investigation of Rocket Exhaust Diffusers for Altitude Simulation", Journal of Propulsion and Power, Vol. 26, No. 2, 2010, pp. 240-247.
DOI
ScienceOn
|
19 |
Shih, T. H. and Lumley, J. L., "Kolmogorov Behavior of Near-Wall Turbulence and its Application in Turbulence Modeling", NASA TM-105663, 1992.
|
20 |
Yang, Z., and Shih, T. H., "New Time Scale Based Model for Near-Wall Turbulence", AIAA Journal, Vol. 31, No. 7, 1993, pp. 1191-1197.
DOI
ScienceOn
|
21 |
Coratekin, T., Keuk, J. V., and Ballmann, J., "Performance of Upwind Scheme and Turbulence Models in Hypersonic Flows", AIAA Journal, Vol. 42, No. 5, 2004, pp. 945-957.
DOI
ScienceOn
|
22 |
Sung, H. G., Unsteady Flowfield in an Integrated Rocket Ramjet Engine and Combustion Dynamics of a Gas Turbine Swirl Stabilized Injector, The Pennsylvania State University, Ph.D. thesis, 1999.
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