High-order shock-fitting methods for direct numerical simulation of hypersonic flow with chemical and thermal nonequilibrium

Prakash, A.; Parsons, N.; Wang, X.; Zhong, X.

doi:10.1016/j.jcp.2011.08.001

High-order shock-fitting methods for direct numerical simulation of hypersonic flow with chemical and thermal nonequilibrium

Journal Article · Thu Sep 01 00:00:00 EDT 2011 · Journal of Computational Physics

DOI:https://doi.org/10.1016/j.jcp.2011.08.001· OSTI ID:1107648

Prakash, A. ^[1]; Parsons, N.; Wang, X.; Zhong, X.

University of California, Los Angeles

In recent years, much progress has been made in the direct numerical simulation of laminar-turbulent transition of hypersonic boundary layer flow. However, most of the efforts at the direct numerical simulation of transition previously have been focused on the idealized perfect gas flow or “cold” hypersonic flows. For practical problems in hypersonic flows, high-temperature effects of thermal and chemical nonequilibrium are important and cannot be modeled by a perfect gas model. Therefore, it is necessary to include the real gas models in the numerical simulation of hypersonic boundary layer transition in order to accurately predict flow field parameters.

Research Organization:: Univ. of California, Los Angeles, CA (United States)

Sponsoring Organization:: USDOE

DOE Contract Number:: FC02-06ER25797

OSTI ID:: 1107648

Report Number(s):: DOE/ER/25797-5

Journal Information:: Journal of Computational Physics, Journal Name: Journal of Computational Physics Journal Issue: 23 Vol. 230; ISSN 0021-9991

Publisher:: Elsevier

Country of Publication:: United States

Language:: English

References (49)

Navier-Stokes solutions with surface catalysis for Martian atmospheric entry Chen, Y. -K; Henline, W. D.; Stewart, D. A. Journal of Spacecraft and Rockets, Vol. 30, Issue 1 https://doi.org/10.2514/3.25468	journal	January 1993
Receptivity of a Hypersonic Flat-Plate Boundary Layer to Three-Dimensional Surface Roughness Wang, Xiaowen; Zhong, Xiaolin Journal of Spacecraft and Rockets, Vol. 45, Issue 6 https://doi.org/10.2514/1.37766	journal	November 2008
Laminar boundary layer stability experiments on a cone at Mach 8. III - Sharp cone at angle of attack Stetson, K.; Thompson, E.; Donaldson, J. 23rd Aerospace Sciences Meeting https://doi.org/10.2514/6.1985-492	conference	January 1985
Receptivity of a supersonic boundary layer over a flat plate. Part 1. Wave structures and interactions Ma, Yanbao; Zhong, Xiaolin Journal of Fluid Mechanics, Vol. 488 https://doi.org/10.1017/S0022112003004786	journal	July 2003
DSMC and Navier-Stokes predictions for hypersonic laminar interacting flows Roy, Christopher; Bartel, Timothy; Gallis, Michael 39th Aerospace Sciences Meeting and Exhibit https://doi.org/10.2514/6.2001-1030	conference	January 2001
Navier-Stokes solutions with surface catalysis for Martian atmospheric entry Chen, Y. -K.; Henline, W.; Stewart, D. 27th Thermophysics Conference https://doi.org/10.2514/6.1992-2946	conference	July 1992
Recommended Collision Integrals for Transport Property Computations Part 1: Air Species Wright, Michael J.; Bose, Deepak; Palmer, Grant E. AIAA Journal, Vol. 43, Issue 12 https://doi.org/10.2514/1.16713	journal	December 2005
Linear disturbances in hypersonic, chemically reacting shock layers Stuckert, Greg; Reed, Helen L. AIAA Journal, Vol. 32, Issue 7 https://doi.org/10.2514/3.12206	journal	July 1994
Comparisons of Transition Prediction Using PSE-Chem to Measurements for a Shock Tunnel Environment MacLean, Matthew; Mundy, Erik; Wadhams, Timothy 37th AIAA Fluid Dynamics Conference and Exhibit https://doi.org/10.2514/6.2007-4490	conference	June 2007
Systematics of Vibrational Relaxation Millikan, Roger C.; White, Donald R. The Journal of Chemical Physics, Vol. 39, Issue 12 https://doi.org/10.1063/1.1734182	journal	December 1963
Transition and Stability of High-Speed Boundary Layers Fedorov, Alexander Annual Review of Fluid Mechanics, Vol. 43, Issue 1 https://doi.org/10.1146/annurev-fluid-122109-160750	journal	January 2011
Implicit total variation diminishing (TVD) schemes for steady-state calculations Yee, H. C.; Warming, R. F.; Harten, A. Journal of Computational Physics, Vol. 57, Issue 3 https://doi.org/10.1016/0021-9991(85)90183-4	journal	February 1985
Leading-edge receptivity to free-stream disturbance waves for hypersonic flow over a parabola Zhong, Xiaolin Journal of Fluid Mechanics, Vol. 441 https://doi.org/10.1017/S0022112001004918	journal	August 2001
Development of a Hybrid Unstructured Implicit Solver for the Simulation of Reacting Flows Over Complex Geometries Nompelis, Ioannis; Drayna, Travis; Candler, Graham 34th AIAA Fluid Dynamics Conference and Exhibit https://doi.org/10.2514/6.2004-2227	conference	June 2012
Receptivity of A Hypersonic Flat-Plate Boundary Layer to Steady Blowing-Suction Wang, Xiaowen; Zhong, Xiaolin 38th Fluid Dynamics Conference and Exhibit https://doi.org/10.2514/6.2008-3731	conference	June 2008
Linear Stability of Hypersonic Flow in Thermochemical Nonequilibrium Hudson, Mary L.; Chokani, Ndaona; Candler, Graham V. AIAA Journal, Vol. 35, Issue 6 https://doi.org/10.2514/2.204	journal	June 1997
Real gas effects on hypersonic boundary‐layer stability Malik, M. R.; Anderson, E. C. Physics of Fluids A: Fluid Dynamics, Vol. 3, Issue 5 https://doi.org/10.1063/1.858012	journal	May 1991
Interaction of Linear Waves with Oblique Shock Waves McKenzie, J. F. Physics of Fluids, Vol. 11, Issue 11 https://doi.org/10.1063/1.1691825	journal	January 1968
Additive Semi-Implicit Runge–Kutta Methods for Computing High-Speed Nonequilibrium Reactive Flows Zhong, Xiaolin Journal of Computational Physics, Vol. 128, Issue 1 https://doi.org/10.1006/jcph.1996.0193	journal	October 1996
Receptivity of a Hypersonic Flat-Plate Boundary Layer to Surface Roughness Wang, Xiaowen; Zhong, Xiaolin 46th AIAA Aerospace Sciences Meeting and Exhibit https://doi.org/10.2514/6.2008-503	conference	January 2008
Numerical Simulation of Weakly Ionized Hypersonic Flow for Reentry Configurations Scalabrin, Leonardo; Boyd, Iain 9th AIAA/ASME Joint Thermophysics and Heat Transfer Conference https://doi.org/10.2514/6.2006-3773	conference	June 2006
Numerical study of hypersonic reacting boundary layer transition on cones Johnson, Heath B.; Seipp, Trevor G.; Candler, Graham V. Physics of Fluids, Vol. 10, Issue 10 https://doi.org/10.1063/1.869781	journal	October 1998
Application of program LAURA to three-dimensional AOTV flowfields Gnoffo, P. 24th Aerospace Sciences Meeting https://doi.org/10.2514/6.1986-565	conference	January 1986
A 3-D non-equilibrium shock-fitting algorithm using effective Rankine-Hugoniot relations Pfitzner, M. 22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference https://doi.org/10.2514/6.1991-1467	conference	June 1991
A Viscosity Equation for Gas Mixtures Wilke, C. R. The Journal of Chemical Physics, Vol. 18, Issue 4 https://doi.org/10.1063/1.1747673	journal	April 1950
Laminar boundary layer stability experiments on a cone at Mach 8. I - Sharp cone Stetson, K.; Thompson, E.; Donaldson, J. 16th Fluid and Plasmadynamics Conference https://doi.org/10.2514/6.1983-1761	conference	July 1983
Hypersonic Real-Gas Effects on Transition Hornung, Hans G. Solid mechanics and its applications https://doi.org/10.1007/978-1-4020-4150-1_32	book	January 2006
Receptivity of a supersonic boundary layer over a flat plate. Part 3. Effects of different types of free-stream disturbances Ma, Yanbao; Zhong, Xiaolin Journal of Fluid Mechanics, Vol. 532 https://doi.org/10.1017/S0022112005003836	journal	June 2005
High-Order Finite-Difference Schemes for Numerical Simulation of Hypersonic Boundary-Layer Transition Zhong, Xiaolin Journal of Computational Physics, Vol. 144, Issue 2 https://doi.org/10.1006/jcph.1998.6010	journal	August 1998
On convergence of computation of chemically reacting flows Park, C. 23rd Aerospace Sciences Meeting https://doi.org/10.2514/6.1985-247	conference	February 2013
Data-Parallel Line Relaxation Method for the Navier-Stokes Equations Wright, Michael J.; Candler, Graham V.; Bose, Deepak AIAA Journal, Vol. 36, Issue 9 https://doi.org/10.2514/2.586	journal	September 1998
Hypersonic laminar–turbulent transition on circular cones and scramjet forebodies Schneider, Steven P. Progress in Aerospace Sciences, Vol. 40, Issue 1-2 https://doi.org/10.1016/j.paerosci.2003.11.001	journal	February 2004
A survey of modern research in hypersonic aerodynamics Anderson, Jr., J. 17th Fluid Dynamics, Plasma Dynamics, and Lasers Conference https://doi.org/10.2514/6.1984-1578	conference	June 1984
Compact finite difference schemes with spectral-like resolution Lele, Sanjiva K. Journal of Computational Physics, Vol. 103, Issue 1 https://doi.org/10.1016/0021-9991(92)90324-R	journal	November 1992
Receptivity of a Supersonic Boundary Layer over a Sharp Wedge to Wall Blowing/Suction Wang, Xiaowen; Zhong, Xiaolin 42nd AIAA Aerospace Sciences Meeting and Exhibit https://doi.org/10.2514/6.2004-254	conference	January 2004
Receptivity to Freestream Disturbances of a Mach 10 Nonequilibrium Reacting Oxygen Flow over a Flat Plate Ma, Yanbao; Zhong, Xiaolin 42nd AIAA Aerospace Sciences Meeting and Exhibit https://doi.org/10.2514/6.2004-256	conference	January 2004
Transition Delay in Hypervelocity Boundary Layers by Means of CO2/Acoustic Instability Interactions Leyva, Ivett; Laurence, Stuart; Beierholm, Amy 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition https://doi.org/10.2514/6.2009-1287	conference	January 2009
Towards the ultimate conservative difference scheme. V. A second-order sequel to Godunov's method van Leer, Bram Journal of Computational Physics, Vol. 32, Issue 1 https://doi.org/10.1016/0021-9991(79)90145-1	journal	July 1979
Nonequilibrium flow computations. I. An analysis of numerical formulations of conservation laws Liu, Yen; Vinokur, Marcel Journal of Computational Physics, Vol. 83, Issue 2 https://doi.org/10.1016/0021-9991(89)90125-3	journal	August 1989
Effect of Nose Bluntness on Hypersonic Boundary Layer Receptivity over a Blunt Cone Zhong, Xiaolin 35th AIAA Fluid Dynamics Conference and Exhibit https://doi.org/10.2514/6.2005-5022	conference	June 2005
Transition Issues for Atmospheric Entry Reshotko, Eli Journal of Spacecraft and Rockets, Vol. 45, Issue 2 https://doi.org/10.2514/1.29777	journal	March 2008
FIRE II Calculations for Hypersonic Nonequilibrium Aerothermodynamics Code Verification: DPLR, LAURA, and US3D Hash, David; Olejniczak, Joseph; Wright, Michael 45th AIAA Aerospace Sciences Meeting and Exhibit https://doi.org/10.2514/6.2007-605	conference	January 2007
Transition on a slender cone in hypervelocity flow Germain, P. D.; Hornung, H. G. Experiments in Fluids, Vol. 22, Issue 3 https://doi.org/10.1007/s003480050036	journal	January 1997
Receptivity of a supersonic boundary layer over a flat plate. Part 2. Receptivity to free-stream sound Ma, Yanbao; Zhong, Xiaolin Journal of Fluid Mechanics, Vol. 488 https://doi.org/10.1017/S0022112003004798	journal	July 2003
Spurious Numerical Oscillations in Simulation of Supersonic Flows Using Shock-Capturing Schemes Lee, Theodore Kai; Zhong, Xiaolin AIAA Journal, Vol. 37, Issue 3 https://doi.org/10.2514/2.732	journal	March 1999
A Review of Transition Studies on Full- Scale Flight Vehicles at Duplicated Flight Conditions in the LENS Tunnels and Comparisons with Prediction Methods and Flight Measurement Wadhams, Timothy; MacLean, Matthew; Holden, Michael 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition https://doi.org/10.2514/6.2010-1246	conference	January 2010
Shock fitting for everybody de Neef, Tom; Moretti, Gino Computers & Fluids, Vol. 8, Issue 3 https://doi.org/10.1016/0045-7930(80)90022-5	journal	September 1980
Self-Consistent Effective Binary Diffusion in Multicomponent Gas Mixtures Ramshaw, J. D. Journal of Non-Equilibrium Thermodynamics, Vol. 15, Issue 3 https://doi.org/10.1515/jnet.1990.15.3.295	journal	January 1990
Critical Hypersonic Aerothermodynamic Phenomena Bertin, John J.; Cummings, Russell M. Annual Review of Fluid Mechanics, Vol. 38, Issue 1 https://doi.org/10.1146/annurev.fluid.38.050304.092041	journal	January 2006

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