Subject
Computational Mathematics
Reference15 articles.
1. G. S. Deiwert, “Supersonic Axisymmetric Flow over Boattails Containing a Centered Propulsive Jet,” AIAA J. 22, 1358–1365 (1984).
2. U. C. Goldberg, J. J. Gorski, and S. R. Chakravarthy, “Afterbody Flowfield Computations at Transonic and Supersonic Mach Numbers,” J. Propulsion Power, No. 1, 56–62 (1987).
3. W. B. Compton III, “Comparison of Turbulence Models for Nozzle-Afterbody Flows with Propulsive Jet,” NASA Tech. Paper, 1996–3592.
4. M. S. Ivanov, D. V. Khotyanovsky, A. N. Kudryavtsev, et al., “Numerical Study of Backflow for Nozzle Plumes Expanding into Vacuum,” AIAA Paper, 2004–2687.
5. E. V. Myshenkov and V. I. Myshenkov, “Numerical Simulation of Efflux from Znamenskii’s Nozzle: Parametric Investigations,” Teplofiz. Vysokikh Temperatur 37, 22–27 (1999) [High Temperature 37, 136–143 (1999)].
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