Silton, S. and Goldstein, D. B., “Numerical and Experimental Investigation of the Reduction of Hypersonic Nose Tip Ablation,” AIAA Paper 98-0169, 36th Aerospace Sciences Meeting, Reno, NV, January 1998.
Silton, S. and Goldstein, D. B., “Numerical and Experimental Investigation of the Reduction of Hypersonic Nose Tip Ablation,” AIAA Paper 98-0169, 36th Aerospace Sciences Meeting, Reno, NV, January 1998.
Roveda, R., Goldstein, D. B. and Varghese, P., “Unsteady Calculation of Slit Flow with a 2-D Hybrid Euler/DSMC Numerical Approach,” AIAA Paper 98-0852, 36th Aerospace Sciences Meeting, Reno, NV, January 1998.
Engblom, W., Goldstein, D. B., Ladoon, D. and Schneider, S., “Fluid Dynamics of Hypersonic Forward-Facing Cavity Flow,” Journal of Spacecraft and Rockets, Vol. 34, No. 4, pp. 437-444, July-Aug. 1997.
Austin, J. V. and Goldstein, D. B., “Direct Numerical Simulation of Circumplanetary Driven Winds on Io,” 29th Annual Meeting of the AAS-DPS, in BAAS, Vol. 29, No. 3, pp. 1004, July 1997.
Roveda, R., Goldstein, D. and Varghese, P., “A Combined Discrete Velocity/Particle Based Numerical Approach for Continuum/Rarefied Flows,” AIAA Paper 97-1006, 35th Aerospace Sciences Meeting, Reno NV, 1997.
Silton, S. and Goldstein, D., “A Preliminary Investigation of Cold Gas Injection into a Forward-Facing Cavity in Hypersonic Flow,” AIAA Paper 97-0705, 35th Aerospace Sciences Meeting, Reno NV, January 1997.
Engblom, W. and Goldstein, D. B., “Nose-Tip Surface Heat Reduction Mechanism,” Journal Thermophysics & Heat Transfer, Vol. 10, No. 4, pp. 598-606, October-December 1996.
Austin, J. V. and Goldstein, D. B., “Direct Numerical Simulation of Pluto’s Extended Atmosphere,” 28th Annual Meeting of the AAS-DPS, in BAAS, Vol. 28, No. 3, pp. 1079, Sept. 1996.
Engblom, W., Yuceil, B., Goldstein, D. B. and Dolling, D. S., “Hypersonic Forward-Facing Cavity Flow: An Experimental and Numerical Study,” Journal of Spacecraft & Rockets, Vol. 33, No. 3, pp. 353-359, May-June, 1996.
Engblom, W. and Goldstein, D. B., “Nose-Tip Surface Heat Reduction Mechanism,” AIAA Paper 96-0354, 34th Aerospace Sciences Meeting, Reno, NV, 1996.