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Relevant bibliographies by topics / Compressible gas dynamics

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Academic literature on the topic 'Compressible gas dynamics'

Author: Grafiati

Published: 4 June 2021

Last updated: 1 February 2022

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Journal articles on the topic "Compressible gas dynamics"

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Mulder, W., S. Osher, and James A. Sethian. "Computing interface motion in compressible gas dynamics." Journal of Computational Physics 100, no. 2 (June 1992): 209–28. http://dx.doi.org/10.1016/0021-9991(92)90229-r.

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Zeidan, D., and H. D. Ng. "Computational methods for gas dynamics and compressible multiphase flows." Shock Waves 29, no. 1 (October 27, 2018): 1–2. http://dx.doi.org/10.1007/s00193-018-0870-9.

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Sciacovelli, L., P. Cinnella, and F. Grasso. "Small-scale dynamics of dense gas compressible homogeneous isotropic turbulence." Journal of Fluid Mechanics 825 (July 21, 2017): 515–49. http://dx.doi.org/10.1017/jfm.2017.415.

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The present paper investigates the influence of dense gases governed by complex equations of state on the dynamics of homogeneous isotropic turbulence. In particular, we investigate how differences due to the complex thermodynamic behaviour and transport properties affect the small-scale structures, viscous dissipation and enstrophy generation. To this end, we carry out direct numerical simulations of the compressible Navier–Stokes equations supplemented by advanced dense gas constitutive models. The dense gas considered in the study is a heavy fluorocarbon (PP11) that is shown to exhibit an inversion zone (i.e. a region where the fundamental derivative of gas dynamics $\unicode[STIX]{x1D6E4}$ is negative) in its vapour phase, for pressures and temperatures of the order of magnitude of the critical ones. Simulations are carried out at various initial turbulent Mach numbers and for two different initial thermodynamic states, one immediately outside and the other inside the inversion zone. After investigating the influence of dense gas effects on the time evolution of mean turbulence properties, we focus on the statistical properties of turbulent structures. For that purpose we carry out an analysis in the plane of the second and third invariant of the deviatoric strain-rate tensor. The analysis shows a weakening of compressive structures and an enhancement of expanding ones. Strong expansion regions are found to be mostly populated by non-focal convergence structures typical of strong compression regions, in contrast with the perfect gas that is dominated by eddy-like structures. Additionally, the contribution of non-focal expanding structures to the dilatational dissipation is comparable to that of compressed structures. This is due to the occurrence of steep expansion fronts and possibly of expansion shocklets which contribute to enstrophy generation in strong expansion regions and that counterbalance enstrophy destruction by means of the eddy-like structures.

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Demkowicz, L., and W. Rachowicz. "On a characteristic finite element method for compressible gas dynamics." International Journal of Engineering Science 25, no. 10 (January 1987): 1259–81. http://dx.doi.org/10.1016/0020-7225(87)90046-2.

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Virk, D., F. Hussain, and R. M. Kerr. "Compressible vortex reconnection." Journal of Fluid Mechanics 304 (December 10, 1995): 47–86. http://dx.doi.org/10.1017/s0022112095004344.

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Reconnection of two antiparallel vortex tubes is studied as a prototypical coherent structure interaction to quantify compressibility effects in vorticity dynamics. Direct numerical simulations of the Navier-Stokes equations for a perfect gas are carried out with initially polytropically related pressure and density fields. For an initial Reynolds number (Re = Γ /v, circulation divided by the kinematic viscosity) of 1000, the pointwise initial maximum Mach number (M) is varied from 0.5 to 1.45. At M=0.5, not surprisingly, the dynamics are essentially incompressible. As M increases, the transfer of Γ starts earlier. For the highest M, we find that shocklet formation between the two vortex tubes enhances early Γ transfer due to viscous cross-diffusion as well as baroclinic vorticity generation. The reconnection at later times occurs primarily due to viscous cross-diffusion for all M. However, with increasing M, the higher early Γ transfer reduces the vortices’ curvature growth and hence the Γ transfer rate; i.e. for the Re case studied, the reconnection timescale increases with M. With increasing M, reduced vortex stretching by weaker ‘bridges’ decreases the peak vorticity at late times. Compressibility effects are significant in countering the stretching of the bridges even at late times. Our observations suggest significantly altered coherent structure dynamics in turbulent flows, when compressible.

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Volkov, K. N., and A. G. Karpenko. "Preconditioning of gas dynamics equations in compressible gas flow computations at low mach numbers." Computational Mathematics and Mathematical Physics 55, no. 6 (June 2015): 1051–67. http://dx.doi.org/10.1134/s0965542515060135.

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Cerminara, M., T. Esposti Ongaro, and L. C. Berselli. "ASHEE: a compressible, Equilibrium–Eulerian model for volcanic ash plumes." Geoscientific Model Development Discussions 8, no. 10 (October 19, 2015): 8895–979. http://dx.doi.org/10.5194/gmdd-8-8895-2015.

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Abstract. A new fluid-dynamic model is developed to numerically simulate the non-equilibrium dynamics of polydisperse gas-particle mixtures forming volcanic plumes. Starting from the three-dimensional N-phase Eulerian transport equations (Neri et al., 2003) for a mixture of gases and solid dispersed particles, we adopt an asymptotic expansion strategy to derive a compressible version of the first-order non-equilibrium model (Ferry and Balachandar, 2001), valid for low concentration regimes (particle volume fraction less than 10−3) and particles Stokes number (St, i.e., the ratio between their relaxation time and flow characteristic time) not exceeding about 0.2. The new model, which is called ASHEE (ASH Equilibrium Eulerian), is significantly faster than the N-phase Eulerian model while retaining the capability to describe gas-particle non-equilibrium effects. Direct numerical simulation accurately reproduce the dynamics of isotropic, compressible turbulence in subsonic regime. For gas-particle mixtures, it describes the main features of density fluctuations and the preferential concentration and clustering of particles by turbulence, thus verifying the model reliability and suitability for the numerical simulation of high-Reynolds number and high-temperature regimes in presence of a dispersed phase. On the other hand, Large-Eddy Numerical Simulations of forced plumes are able to reproduce their observed averaged and instantaneous flow properties. In particular, the self-similar Gaussian radial profile and the development of large-scale coherent structures are reproduced, including the rate of turbulent mixing and entrainment of atmospheric air. Application to the Large-Eddy Simulation of the injection of the eruptive mixture in a stratified atmosphere describes some of important features of turbulent volcanic plumes, including air entrainment, buoyancy reversal, and maximum plume height. For very fine particles (St → 0, when non-equilibrium effects are negligible) the model reduces to the so-called dusty-gas model. However, coarse particles partially decouple from the gas phase within eddies (thus modifying the turbulent structure) and preferentially concentrate at the eddy periphery, eventually being lost from the plume margins due to the concurrent effect of gravity. By these mechanisms, gas-particle non-equilibrium processes are able to influence the large-scale behavior of volcanic plumes.

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Khaytaliev, Ismatolo Ramazanovich, and Evgeny Vladimirovich Shilnikov. "Investigation of the properties of a quasi-gas-dynamic system of equations based on the solution of the Riemann problem for a mixture of gases." Keldysh Institute Preprints, no. 52 (2021): 1–12. http://dx.doi.org/10.20948/prepr-2021-52.

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The accuracy and stability of an explicit numerical algorithm for modeling the flows of a mixture of compressible gases in the transonic regime are investigated by the example of solving the Riemann problem on the decay of a gas-dynamic discontinuity between different gases. The algorithm is constructed using the finite volume method based on the regularized gas dynamics equations for a mixture of gases. A method for suppressing nonphysical oscillations occurring behind the contact discontinuity is found.

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Schamel, Hans. "Lagrangian fluid description with simple applications in compressible plasma and gas dynamics." Physics Reports 392, no. 5 (March 2004): 279–319. http://dx.doi.org/10.1016/j.physrep.2003.12.002.

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GLAISTER, P. "A Shock-Reflection Problem in Compressible-Gas Dynamics with a Similarity Solution." IMA Journal of Numerical Analysis 8, no. 3 (1988): 343–56. http://dx.doi.org/10.1093/imanum/8.3.343.

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Dissertations / Theses on the topic "Compressible gas dynamics"

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Rudgyard, Michael A. "Cell vertex methods for compressible gas flows." Thesis, University of Oxford, 1990. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.279991.

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Jiang, Ning. "Weakly compressible Navier-Stokes approximation of gas dynamics." College Park, Md. : University of Maryland, 2006. http://hdl.handle.net/1903/3883.

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Thesis (Ph. D.) -- University of Maryland, College Park, 2006.
Thesis research directed by: Mathematics. Title from t.p. of PDF. Includes bibliographical references. Published by UMI Dissertation Services, Ann Arbor, Mich. Also available in paper.

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Andrews, J. G. "An a posteriori error indicator and its application to adaptive methods in CFD." Thesis, University of Oxford, 1996. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.319051.

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Ahmed, Shafkat. "Interactions of Gas Particles with Graphene during Compressible Flow Exfoliation: A Molecular Dynamics Simulations Study." University of Toledo / OhioLINK, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=toledo1588278674983556.

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Barnes, Caleb J. "An Implicit High-Order Spectral Difference Method for the Compressible Navier-Stokes Equations Using Adaptive Polynomial Refinement." Wright State University / OhioLINK, 2011. http://rave.ohiolink.edu/etdc/view?acc_num=wright1315591802.

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Pretorius, Johannes Jacobus. "A network approach for the prediction of flow and flow splits within a gas turbine combustor." Diss., University of Pretoria, 2005. http://hdl.handle.net/2263/26712.

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The modern gas turbine engine industry needs a simpler and faster method to facilitate the design of gas turbine combustors due to the enormous costs of experimental test rigging and detailed computational fluid dynamics (CFD) simulations. Therefore, in the initial design phase, a couple of preliminary designs are conducted to establish initial values for combustor performance and geometric characteristics. In these preliminary designs, various one-dimensional models using analytical and empirical formulations may be used. One of the disadvantages of existing models is that they are typically geometric dependant, i.e. they apply only to the geometry they are derived for. Therefore the need for a more versatile design tool exists. In this work, which constitutes the first step in the development of such a versatile design tool, a single equation-set network simulation model to describe both steady state compressible and incompressible isothermal flow is developed. The continuity and momentum equations are solved through a hybrid type network model analogy which makes use of the SIMPLE pressure correction methodology. The code has the capability to efficiently compute flow through elements where the loss factor K is highly flow dependant and accurately describes variable area duct flow in the case of incompressible flow. The latter includes ducts with discontinuously varying flow sectional areas. Proper treatment of flow related non-linearities, such as flow friction, is facilitated in a natural manner in the proposed methodology. The proposed network method is implemented into a Windows based simulation package with a user interface. The ability of the proposed method to accurately model both compressible and incompressible flow is demonstrated through the analyses of a number of benchmark problems. It will be shown that the proposed methodology yields similar or improved results as compared to other’s work. The proposed method is applied to a research combustor to solve for isothermal flows and flow splits. The predicted flows were in relatively close agreement with measured data as well as detailed CFD analysis.
Dissertation (MEng (Mechanical Engineering))--University of Pretoria, 2005.
Mechanical and Aeronautical Engineering
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Virdi, Amandeep Singh. "Aero-thermal performance and enhanced internal cooling of unshrouded turbine blade tips." Thesis, University of Oxford, 2015. https://ora.ox.ac.uk/objects/uuid:62c3e94a-a1ff-47a8-bb81-e870b0013f11.

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The tips of unshrouded, high-pressure turbine blades are prone to significantly high heat loads. The gap between the tip and over-tip casing is the root cause of undesirable over-tip leakage flow that is directly responsible for high thermal material degradation and is a major source of aerodynamic loss within a turbine. Both must be minimised for the safe working and improved performance of future gas-turbines. A joint experimental and numerical study is presented to understand and characterise the heat transfer and aerodynamics of unshrouded blade tips. The investigation is undertaken with the use of a squealer or cavity tip design, known for offering the best overall compromise between the tip aerodynamics, heat transfer and mechanical stress. Since there is a lack of understanding of these tips at engine-realistic conditions, the present study comprises of a detailed analysis using a high-speed linear cascade and computational simulations. The aero-thermal performance is studied to provide a better insight into the behaviour of squealer tips, the effects of casing movement and tip cooling. The linear cascade environment has proved beneficial for its offering of spatially-resolved data maps and its ability to validate computational results. Due to the unknown tip gap height within an entire engine cycle, the effects of gap height are assessed. The squealer's aero-thermal performance has been shown to be linked with the gap height, and qualitative different trends in heat transfer are established between low-speed and high-speed tip flow regimes. To the author's knowledge, the present work is the first of its kind, providing comprehensive aero-thermal experimental research and a dataset for a squealer tip at engine-representative transonic conditions. It is also unique in terms of conducting direct and systematic validations of a major industrial computational fluid dynamics method for aero-thermal performance prediction of squealer tips at enginerepresentative transonic conditions. Finally, after recognising the highest heat loads are found on the squealer rims, a novel shaped squealer tip has been investigated to help improve the thermal performance of the squealer with a goal to improve its durability. It has been discovered that a seven percent reduction in tip temperature can be achieved through incorporating a shaped squealer and maximising the internal cooling performance.

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Yassine, Mohamad. "Multi-physics modeling of the intake line of an internal combustion engine." Thesis, Ecole centrale de Nantes, 2019. http://www.theses.fr/2019ECDN0005.

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La concurrence entre les constructeurs automobiles pour introduire les solutions les plus innovantes est de plus en plus importante. Depuis quelques années, la simulation est largement utilisée dans le domaine d’automobile. Concernant l’étude de la dynamique des gaz et de la propagation des ondes de pression dans le système d’admission d’un moteur à combustion interne, qui ont des effets significatifs sur le comportement du moteur, une modélisation précise est nécessaire afin d’obtenir de bons résultats. L’objectif principal de la méthodologie présentée dans cette thèse est de réduire le temps de simulation permettant d’étudier le fonctionnement de moteurs à combustion interne tout en conservant un bon niveau de précision. Les ondes de pression ont été étudiées en utilisant une approche fréquentielle. Cette dernière est basée sur une fonction de transfert, qui relie la pression relative au débit masse d’air en amont de la soupape d'admission. Un couplage multi-physique avec le logiciel de simulation a été établi. La validation du modèle a été effectuée à l'aide d'un critère de précision relatif au rendement volumétrique et à la pression instantanée en amont de la soupape d'admission. Les résultats ont montré un bon niveau précision. En termes de temps de calcul, la méthodologie de la fonction de transfert est plus rapide que le code de simulation natif. Cette méthodologie peut être une méthode alternative pour modéliser la géométrie d’admission d'un moteur à combustion interne
The competition among carmakers to introduce the most innovative solutions is growing day by day. Since few years, simulation is being used widely in automotive industries. Concerning the study of gas dynamics and pressure wave’s propagation in the intake system of an internal combustion engine, whichhave a significant effect on engine behavior, a precise modelling is needed in order to obtain good results. The main objective of the methodology presented in this PhD thesis, is to shorten the simulation time in order to study the behavior of an internal combustion engine, while conserving a good accuracy level. The pressure waves are studied using frequency approach. This latter is based on a transfer function, which links the relative pressure and the air mass flow rate upstream the intake valve. A multi-physics coupling model in the simulation code was established. The model validation was conducted using precision criterion on volumetric efficiency and on instantaneous pressure upstream of the intake valve. The results showed good accuracy level. In terms of computational time, the transfer function methodology is faster than the native one-dimensional non-linear code. This methodology can be an alternative method for modeling the intake geometry of an IC engine

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Chisum, James E. "Simulation of the dynamic behavior of explosion gas bubbles in a compressible fluid medium." Diss., Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 1996. http://handle.dtic.mil/100.2/ADA326363.

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Dissertation (Ph.D. in Mechanical Engineering) Naval Postgraduate School, December 1996.
Dissertation supervisor(s): Young S. Shin. "December 1996." Includes bibliographical references (p. 81-83). Also available online.

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Corot, Théo. "Simulation numérique d'ondes de choc dans un milieu bifluide : application à l'explosion vapeur." Thesis, Paris, CNAM, 2017. http://www.theses.fr/2017CNAM1125/document.

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Cette thèse s'intéresse à la simulation numérique de l'explosion vapeur. Ce phénomène correspond à une vaporisation instantanée d'un volume d'eau liquide entraînant un choc de pression. Nous nous y intéressons dans le cadre de la sûreté nucléaire. En effet, lors d'un accident entraînant la fusion du cœur du réacteur, du métal fondu pourrait interagir avec de l'eau liquide et entraîner un tel choc. On voudrait alors connaître l'ampleur de ce phénomène et les risques d'endommagements de la centrale qu'il implique. Pour y parvenir, nous utilisons pour modèle les équations d'Euler dans un cadre Lagrangien. Cette description a l'avantage de suivre les fluides au cours du temps et donc de parfaitement conserver les interfaces entre l'eau liquide et sa vapeur. Pour résoudre numériquement les équations obtenues, nous développons un nouveau schéma de type Godunov utilisant des flux nodaux. Le solveur nodal développé durant cette thèse ne dépend que de la répartition angulaire des variables physiques autour du nœud. De plus, nous nous intéressons aux changements de phase liquide-vapeur. Nous proposons une méthode pour les prendre en compte et mettons en avant les avantages qu'il y a à l'implémentation de ce phénomène dans un algorithme Lagrangien
This thesis studies numerical simulation of steam explosion. This phenomenon correspond to a fast vaporization of a liquid leading to a pressure shock. It is of interest in the nuclear safety field. During a core-meltdown crisis, molten fuel rods interacting with water could lead to steam explosion. Consequently we want to evaluate the risks created by this phenomenon.In order to do it, we use Euler equations written in a Lagrangian form. This description has the advantage of following the fluid motion and consequently preserves interfaces between the liquid and its vapor. To solve these equations, we develop a new Godunov type scheme using nodal fluxes. The nodal solver developed here only depends on the angular repartition of the physical variables around the node.Moreover, we study liquid-vapor phase changes. We describe a method to take it into account and highlight the advantages of using this method into a Lagrangian framework

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Books on the topic "Compressible gas dynamics"

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Modern compressible flow: With historical perspective. 3rd ed. Boston: McGraw-Hill, 2003.

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Modern compressible flow: With historical perspective. 2nd ed. New York: McGraw-Hill, 1990.

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Husain, Zoeb. Compressible flow through problems or gas dynamics through problems. New York: Wiley, 1989.

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Perthame, B. On positively preserving finite volume schemes for compressible Euler Equations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

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Perthame, Benoit. On positively preserving finite volume schemes for compressible Euler Equations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

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Wong, C. Channy. A domain decomposition study of massively parallel computing in compressible gas dynamics. Washington: American Institute of Aeronautics and Astronautics, 1995.

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Xu, Kun. A gas-kinetic BGK scheme for the compressible Navier-Stokes equations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2000.

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Lui, Shiu-Hong. Entropy analysis of kinetic flux vector splitting schemes for the compressible Euler equations. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1999.

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Chisum, James E. Simulation of the dynamic behavior of explosion gas bubbles in a compressible fluid medium. Monterey, Calif: Naval Postgraduate School, 1996.

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Anderson, John. Modern Compressible Flow. OPEN UNIVERSITY PRES, 2004.

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Book chapters on the topic "Compressible gas dynamics"

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Achterberg, Abraham. "Steady, Ideal Compressible Flows." In Gas Dynamics, 103–23. Paris: Atlantis Press, 2016. http://dx.doi.org/10.2991/978-94-6239-195-6_6.

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Sasoh, Akihiro. "Motion of Gas Particles and Thermodynamics." In Compressible Fluid Dynamics and Shock Waves, 13–39. Singapore: Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-0504-1_2.

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Shyue, Keh-Ming. "An Eulerian Interface-Sharpening Algorithm for Compressible Gas Dynamics." In Modeling, Simulation and Optimization of Complex Processes - HPSC 2012, 221–31. Cham: Springer International Publishing, 2014. http://dx.doi.org/10.1007/978-3-319-09063-4_18.

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Després, Bruno, and Emmanuel Labourasse. "Towards stabilization of cell-centered Lagrangian methods for compressible gas dynamics." In Finite Volumes for Complex Applications VI Problems & Perspectives, 323–29. Berlin, Heidelberg: Springer Berlin Heidelberg, 2011. http://dx.doi.org/10.1007/978-3-642-20671-9_34.

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Giauque, Alexis, Aurélien Vadrot, Paolo Errante, and Christophe Corre. "Towards Subgrid-Scale Turbulence Modeling in Dense Gas Flows." In Proceedings of the 3rd International Seminar on Non-Ideal Compressible Fluid Dynamics for Propulsion and Power, 71–77. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-69306-0_8.

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Winn, Stephen D., and Emile Touber. "Non-ideal Gas Effects on Supersonic-Nozzle Transfer Functions." In Proceedings of the 3rd International Seminar on Non-Ideal Compressible Fluid Dynamics for Propulsion and Power, 12–19. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-69306-0_2.

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Reinker, Felix, Robert Wagner, Max Passmann, Leander Hake, and Stefan aus der Wiesche. "Performance of a Rotatable Cylinder Pitot Probe in High Subsonic Non-ideal Gas Flows." In Proceedings of the 3rd International Seminar on Non-Ideal Compressible Fluid Dynamics for Propulsion and Power, 144–52. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-69306-0_15.

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Dolzhansky, Felix V. "The Rossby–Obukhov Potential Vortex; Energy and Momentum of a Compressible Fluid; Hydrodynamic Approximation of Equations of Gas Dynamics." In Fundamentals of Geophysical Hydrodynamics, 31–39. Berlin, Heidelberg: Springer Berlin Heidelberg, 2013. http://dx.doi.org/10.1007/978-3-642-31034-8_4.

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Skews, B. W., M. D. Atkins, and M. W. Seitz. "Gas dynamic and physical behaviour of compressible porous foams struck by a weak shock wave." In Shock Waves, 511–16. Berlin, Heidelberg: Springer Berlin Heidelberg, 1992. http://dx.doi.org/10.1007/978-3-642-77648-9_80.

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"Compressible Flow Equations." In Applied Gas Dynamics, 221–37. Chichester, UK: John Wiley & Sons, Ltd, 2019. http://dx.doi.org/10.1002/9781119500377.ch5.

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Conference papers on the topic "Compressible gas dynamics"

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Kustova, E. V., E. A. Nagnibeda, D. Giordano, and Takashi Abe. "Chemical-Reaction Rates in Non-equilibrium Viscous Compressible Flows." In RARIFIED GAS DYNAMICS: Proceedings of the 26th International Symposium on Rarified Gas Dynamics. AIP, 2008. http://dx.doi.org/10.1063/1.3076584.

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Ohwada, Taku. "Boltzmann schemes for the compressible Navier-Stokes equations." In RAREFIED GAS DYNAMICS: 22nd International Symposium. AIP, 2001. http://dx.doi.org/10.1063/1.1407578.

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Sielemann, Michael. "High-Speed Compressible Flow and Gas Dynamics." In 9th International MODELICA Conference, Munich, Germany. Linköping University Electronic Press, 2012. http://dx.doi.org/10.3384/ecp1207681.

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Sakurai, Akira. "A compressible turbulent flow in a molecular kinetic gas model." In RAREFIED GAS DYNAMICS: 22nd International Symposium. AIP, 2001. http://dx.doi.org/10.1063/1.1407553.

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Fronzeo, Melissa, and Michael P. Kinzel. "An Investigation of Compressible Gas Jets Submerged Into Water." In 46th AIAA Fluid Dynamics Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2016. http://dx.doi.org/10.2514/6.2016-4253.

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Skovorodko, P. A. "Slip effects in compressible turbulent channel flow." In 28TH INTERNATIONAL SYMPOSIUM ON RAREFIED GAS DYNAMICS 2012. AIP, 2012. http://dx.doi.org/10.1063/1.4769570.

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Combe, Laure, Jean-Marc Herard, Laure Combe, and Jean-Marc Herard. "A finite volume algorithm to compute dense compressible gas-solid flows." In 13th Computational Fluid Dynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1997. http://dx.doi.org/10.2514/6.1997-2082.

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Xu, Kun, and Antony Jameson. "Gas-kinetic relaxation (BGK-type) schemes for the compressible Euler equations." In 12th Computational Fluid Dynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1995. http://dx.doi.org/10.2514/6.1995-1736.

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Jain, Vaibhav, and Chengxian Lin. "Effects of Aspect Ratio on Compressible Gas Flow in Microchannels." In 36th AIAA Fluid Dynamics Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2006. http://dx.doi.org/10.2514/6.2006-3717.

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Bergen, Benjamin K., Marcus G. Daniels, and Paul M. Weber. "A Hybrid Programming Model for Compressible Gas Dynamics Using OpenCL." In 2010 International Conference on Parallel Processing Workshops (ICPPW). IEEE, 2010. http://dx.doi.org/10.1109/icppw.2010.60.

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