Access provided by Rice University


S. L. Gai, N. T. Reynolds, C. Ross, and J. P. Baird. Measurements of heat transfer in separated high-enthalpy dissociated laminar hypersonic flow behind a step. Journal of Fluid Mechanics, 199:541-561, 1989.
CrossRef
M. J. Hayne, S. L. Gai, R. Hillier, R. G. Morgan, D. J. Mee, and T. J. McIntyre. Heat transfer and flow behind a rearward facing step in a super-orbital expansion tube. In 23rd international symposium on shock waves, 22-27 July 2002, Fort Worth, Texas, USA, In: Lu,F.K., editor, Fort Worth, University of Texas, 2002, Pages: 1574-1580, pages 1574-1580, July 2002.
M. J. Hayne. Hypervelocity Flow Over Rearward-Facing Steps. PhD thesis, Department of Mechanical Engineering, University of Queensland, March 2004.
Michael S. Holden. Establishment time of laminar separated flows. AIAA Journal, 9(11):2296-2298, 1971.
CrossRef
Josef Rom and Arnan Seginer. Laminar heat transfer to a two-dimensional backward facing step from the high-enthalpy supersonic flow in the shock tube. AIAA Journal, 2(2):251-255, Feb 1964.
CrossRef
S. L. Gai, M. J. Hayne, A. D. Gardner, R. G. Morgan, and D. J. Mee. Heat transfer behind a step in high enthalpy super-orbital flow. In Proceedings of the 39th Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan 2001.
P. A. Jacobs. Mb-cns: a computer program for the simulation of transient compressible flows. Technical Report Report 10/96, Department of Mechanical Engineering, University of Queensland, Brisbane, December 1996.
P. A. Jacobs and R. J. Gollan. The eilmer3 code. Technical Report Report 2008/07, Department of Mechanical Engineering, University of Queensland, Brisbane, May 2010.
Chul Park. Review of chemical-kinetic problems of future nasa missions, i: Earth entries. Journal of Thermophysics and Heat Transfer, 7(3), July-Sept 1993.
W. K. Anderson and J. L. Thomas. A comparison of finite volume flux vector splittings for the euler equations. AIAA, 24(9):1453-1460, 1986.
CrossRef
Y. Wada and M. S. Liou. A flux splitting scheme with high-resolution and robustness for discontinuities. In Aerospace Sciences Meeting and Exhibit, 32nd, Reno, NV, Jan 10-13, 1994, number AIAA-1994-83, 1994.
P. A. Jacobs. Single-block navier-stokes integrator. Technical Report ICASE Interim Report 18, NASA Langley Research Center, Hampton, VA, July 1991.
P. A. Jacobs. Numerical simulation of transient hypervelocity flow in an expansion tube. Computers & Fluids, 23(1):77-101, Jan 1994.
CrossRef
I. A. Johnston. Simulation of Flow Around Hypersonic Blunt-Nosed Vehicles for the Calibration of Air Data Systems. PhD thesis, Department of Mechanical Engineering, University of Queensland, Jan 1999.
I. A. Johnston, S. L. Tuttle, P. A. Jacobs, and T. Shimoda. The numerical and experimental simulation of hypervelocity flow around the hyflex vehicle forebody. Shock Waves, 9(1):57-67, Feb 1999.
CrossRef
V. Wheatley, H. S. Chiu, P. A. Jacobs, M. N. Macrossan, D. J. Mee, and R. G. Morgan. Rarefied, superorbital flows in an expansion tube. International Journal of Numerical Methods for Heat & Fluid Flow, 14(4):512-537, 2004.
CrossRef
P. A. Jacobs, T. B. Silvester, R. G. Morgan, M. P. Scott, R. J. Gollan, and T. J. McIntyre. Superorbital expansion tube operation:estimates of flow conditions via numerical simulation. In 43rd AIAA Aerospace Sciences Meeting and Exhibit, 10-13 January 2005, Reno, Nevada. AIAA, 2005.
Mpi: A message-passing interface standard, 2009.
Roop N. Gupta, Jerrold M. Yos, Richard A. Thompson, and Kam-Pui Lee. A review of reaction rates and thermodynamic and transport properties for an 11-species air model for chemical and thermal nonequilibrium calculations to 30 000 k. Technical Report 1232, NASA, 1990.
G. R. S. Sarma. Physico-chemical modelling in hypersonic flow simulation. Progress in Aerospace Sciences, 36(3-4):281-349, April 2000.
CrossRef
Druguet. M. C, G. Ben-Dor, and D. Zeitoun. The interaction of supersonic and hypersonic flows with a double cone: comparison between inviscid, viscous, perfect and real gas model simulations. In 26th International Symposium on Shock Waves, Gottingen, Germany, volume 2, pages 1527-1532, July 2007.
Ghislain Tchuen and David E. Zeitoun. Effects of chemistry in nonequilibrium hypersonic flow around blunt bodies. Journal of Thermophysics and Heat Transfer, 23(3):433-442, July-Sept 2009.
CrossRef
Ioannis Nompelis, Graham V. Candler, Matthew MacLean, Timothy P. Wadhams, and Michael S. Holden. Numerical investigation of double-cone flow experiments with high-enthalpy effects. In 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition in Orlando, Florida, 4-7 Jan 2010, number AIAA 2010-1283. AIAA, Jan 2010.
G. Park, S. L. Gai, and A. J. Neely. Aerothermodynamics behind a blunt boday at superorbital speeds. AIAA Journal, 48(8):1804-1816, 2010.
CrossRef
S. Gordon and B. J. McBride. Computer program for calculation of complex chemical equilibrium compositions and applications: I analysis. Technical Report NASA Reference Publication 1311, NASA, 1994.
Rowan J. Gollan. Yet another finite-rate chemistry module for compressible flow codes. Technical Report Division Report, Department of Mechanical Engineering, University of Queensland, Brisbane, July 2003.
David Ray Mott. New Quasi-Steady-State and Partial-Equilibrium Methods for Integrating Chemically Reacting Systems. PhD thesis, The University of Michigan, 1999.
ICEM-CFD. Ansys icem cfd., 2008, ansys inc, southpointe 275 technology drive canonsburg, pa 15317, usa, 2008.
A. P. Jackson, R. Hillier, and S. Soltani. Experimental and computational study of laminar cavity flows at hypersonic speeds. Journal of Fluid Mechanics, 427:329-358, 2001.
CrossRef
P. J. Roache. Quantification of uncertainty in computational fluid dynamics. Annual Review of Fluid Mechanics, 29:123-160, 1997.
CrossRef
AIAA. Policy statement on numerical accuracy and experimental uncertainty. AIAA Journal, 32(1):3 (editorial), 1994.
P. J Roache, K. N. Ghia, and F. M. White. Editorial policy statement on the control of numerical accuracy. ASME Journal of Fluids Engineering, 108:2, 1986.
CrossRef
M. J. Hayne, D. J. Mee, R. G. Morgan, S. L. Gai, and T. J. McIntyre. Heat transfer and flow behind a step in high enthalpy superorbital flow. The Aeronautical Journal, (2778):435-442, July 2003.
S. Goldstein. On laminar boundary-layer flow near a position of separation. Quart. J. Mech. Applied Math., 1:43-69, 1946.
CrossRef
K. Stewartson. On the flow near the trailing edge of a flat plate. Proc. Roy. Soc. A., 306(1486):275-290, Sept 1968.
CrossRef
A. F. Messiter. Boundary layer flow near the trailing edge of flat plate. SIAM J. Appl. Math., 18:241-257, 1970.
CrossRef
P. G. Daniels. Numerical and asymptotic solutions for the supersonic flow near the trailing edge of a flat plate. Quart. J. Mech. Applied Math., XXVII(2):175-191, 1974.
Francis R. Hama. Experimental studies on the lip shock. AIAA Journal, 6(2):212-219, Feb 1968.
CrossRef
S. Weinbaum. On the singular points in the laminar two-dimensional near wake flow field. Journal of Fluid Mechanics, 33(1):39-63, 1968.
CrossRef
M. J. Hayne, D. J. Mee, S. L. Gai, and T .J. McIntyre. Boundary layers on a flat plate at sub-and superorbital speeds. Journal of Thermophysics and Heat Transfer, 21(4):772-779, Oct-Dec 2007.
CrossRef