Academic literature on the topic 'Ideal gas flow'

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Journal articles on the topic "Ideal gas flow"

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Sun, Wenjing, Wenqi Zhong, and Jingzhou Zhang. "Experimental Investigation on Turbulent Flow Deviation in a Gas-Particle Corner-Injected Flow." Processes 9, no. 12 (2021): 2202. http://dx.doi.org/10.3390/pr9122202.

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An experimental model of a corner-injected flow is built to investigate the turbulent flow behavior by employing the PIV technique. The influences of the ideal tangential circle, the additive particles and the initial gas mass flux on the corner-injected flow are analyzed systematically. To be specific, the flow deviation, the velocity profile, the vortex evolution and the turbulent flow development are discussed quantitatively. The influences of the increasing ideal tangential circle on the turbulent jet deviation are shortened gradually, and the impinging circles are obviously narrowed with
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WANG, Moran. "Similarity of ideal gas flow at different scales." Science in China Series E 46, no. 6 (2003): 661. http://dx.doi.org/10.1360/02ye0072.

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Cornelius, Kenneth C., and Kartik Srinivas. "Isentropic Compressible Flow for Non-Ideal Gas Models for a Venturi." Journal of Fluids Engineering 126, no. 2 (2004): 238–44. http://dx.doi.org/10.1115/1.1677499.

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The non-ideal gas equations and mathematical formulation developed in this work using the compressibility factor in the equation of state closely resemble the derivations used for the ideal gas mathematical formulation for a direct comparison of the differences between the ideal versus the non-ideal gas law. The local Mach number is defined for the non-ideal gas. The plenum total variables used in compressible flow are expressed in terms of the local Mach number for the polytrope and Rayleigh models. A power law relationship is derived between the thermodynamic variables that allow an analytic
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Dias, Frédéric, Alan R. Elcrat, and Lloyd N. Trefethen. "Ideal jet flow in two dimensions." Journal of Fluid Mechanics 185 (December 1987): 275–88. http://dx.doi.org/10.1017/s0022112087003173.

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A jet is a stream of one fluid entering another at high speed. In the simplest classical model of jet flow, the geometry is two-dimensional, gravity and viscosity are ignored, the moving fluid is a liquid, and the stationary fluid is a gas whose influence is assumed negligible. The description of this idealized flow can be reduced to a problem of complex analysis, but, except for very simple nozzle geometries, that problem cannot be solved analytically. This paper presents an efficient procedure for solving the jet problem numerically in the case of an arbitrary polygonal nozzle.
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Zhitnikov, V. P., and A. G. Terent'ev. "Axisymmetric flow of ideal fluid past a gas bubble." Fluid Dynamics 28, no. 5 (1994): 667–71. http://dx.doi.org/10.1007/bf01050050.

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Hołyst, Robert, Paweł J. Żuk, Anna Maciołek, Karol Makuch, and Konrad Giżyński. "Direction of Spontaneous Processes in Non-Equilibrium Systems with Movable/Permeable Internal Walls." Entropy 26, no. 8 (2024): 713. http://dx.doi.org/10.3390/e26080713.

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We consider three different systems in a heat flow: an ideal gas, a van der Waals gas, and a binary mixture of ideal gases. We divide each system internally into two subsystems by a movable wall. We show that the direction of the motion of the wall, after release, under constant boundary conditions, is determined by the same inequality as in equilibrium thermodynamics dU−đQ≤0. The only difference between the equilibrium and non-equilibrium laws is the dependence of the net heat change, đQ, on the state parameters of the system. We show that the same inequality is valid when introducing the gra
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Almeida, Alcino R. "A Model To Calculate the Theoretical Critical Flow Rate Through Venturi Gas Lift Valves." SPE Journal 16, no. 01 (2010): 134–47. http://dx.doi.org/10.2118/126184-pa.

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Summary A model to calculate the theoretical critical flow rate of nitrogen (N2) or natural gas through a Venturi gas lift valve is described herein. This new model considers real-gas effects not only in density calculations but also in other thermodynamic properties that are relevant during gas isentropic evolution. For the properties of N2, the Bennedict, Webb, and Rubin (BWR) equation of state and an accurate correlation for the ideal-gas isobaric heat capacity were used. For natural gas, the Dranchuk and Abou-Kassem equation, which reproduces the well-known Standing and Katz chart, was use
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Anand, R. K. "Jump relations across a shock in non-ideal gas flow." Astrophysics and Space Science 342, no. 2 (2012): 377–88. http://dx.doi.org/10.1007/s10509-012-1175-6.

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Sirignano, William A. "Compressible flow at high pressure with linear equation of state." Journal of Fluid Mechanics 843 (March 21, 2018): 244–92. http://dx.doi.org/10.1017/jfm.2018.166.

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Compressible flow varies from ideal-gas behaviour at high pressures where molecular interactions become important. It is widely accepted that density is well described through a cubic equation of state while enthalpy and sound speed are functions of both temperature and pressure, based on two parameters, $A$ and $B$, related to intermolecular attraction and repulsion, respectively. Assuming small variations from ideal-gas behaviour, a closed-form approximate solution is obtained that is valid over a wide range of conditions. An expansion in these molecular interaction parameters simplifies rel
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Elmar Agayev, Elmar Agayev. "THE STUDY OF LAMINAR AND TURBULENT FLOW IN TURBINE TYPE OF FLOW METERS." PIRETC-Proceeding of The International Research Education & Training Centre 27, no. 06 (2023): 140–49. http://dx.doi.org/10.36962/piretc27062023-140.

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The paper studies the operation of a turbine-type flow meter under various operating modes. In the industry, flow measuring devices are widely used on oil and gas platforms and terminals. In the processes of production, processing and transportation of oil and gas, which is a strategic raw material, strict state control of its consumption is carried out precisely by means of consumption measurement. A performance study has been carried out for turbine - type gas flow meters under laminar and turbulent gas flow conditions .. One of the main factors that cause damage to the mechanical parts of t
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Dissertations / Theses on the topic "Ideal gas flow"

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Bates, Dana Michelle. "On a free boundary problem for ideal, viscous and heat conducting gas flow." Diss., University of Iowa, 2016. https://ir.uiowa.edu/etd/2180.

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We consider the flow of an ideal gas with internal friction and heat conduction in a layer between a fixed plane and an upper free boundary. We describe the top free surface as the graph of a time dependent function. This forces us to exclude breaking waves on the surface. For this and other reasons we need to confine ourselves to flow close to a motionless equilibrium state which is fairly easy to compute. The full equations of motion, in contrast to that, are quite difficult to solve. As we are close to an equilibrium, a linear system of equations can be used to approximate the behavior of t
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Shokina, Nina Yurievna. "Numerical modelling of multi-dimensional steady ideal gas and fluid flows." [S.l. : s.n.], 2000. http://elib.tu-darmstadt.de/diss/000101/newphd.pdf.

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Shokina, Nina Yurievna. "Numerical Modelling of Multi-dimensional Steady Ideal Gas and Fluid Flows." Phd thesis, 2001. http://tuprints.ulb.tu-darmstadt.de/101/1/newphd.pdf.

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The thesis is devoted to the numerical modelling of two- and three-dimensional ideal fluid flows in channels of complicated geometries on the basis of the adaptive grid method. Iterative finite difference methods for the numerical modelling of ideal gas and fluid flows are developed using new dependent variables. For two-dimensional flows these variables are stream function and vorticity function, for three-dimensional flows these variables are: vector potential and vorticity vector. The set of equations for the stream function and vorticity, for which the appropriate boundary conditions are t
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Zingan, Valentin Nikolaevich. "Discontinuous Galerkin Finite Element Method for the Nonlinear Hyperbolic Problems with Entropy-Based Artificial Viscosity Stabilization." Thesis, 2012. http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-10845.

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This work develops a discontinuous Galerkin finite element discretization of non- linear hyperbolic conservation equations with efficient and robust high order stabilization built on an entropy-based artificial viscosity approximation. The solutions of equations are represented by elementwise polynomials of an arbitrary degree p > 0 which are continuous within each element but discontinuous on the boundaries. The discretization of equations in time is done by means of high order explicit Runge-Kutta methods identified with respective Butcher tableaux. To stabilize a numerical solution in the
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Shokina, Nina Yurievna [Verfasser]. "Numerical modelling of multi-dimensional steady ideal gas and fluid flows / vorgelegt von Nina Yurievna Shokina." 2000. http://d-nb.info/96272906X/34.

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Books on the topic "Ideal gas flow"

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Center, Ames Research, ed. Steady secondary flows generated by periodic compression and expansion of an ideal gas in a pulse tube. National Aeronautics and Space Administration, Ames Research Center, 1999.

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Witte, David W. Computer code for determination of thermally perfect gas properties. National Aeronautics and Space Administration, Langley Research Center, 1994.

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E, Tatum Kenneth, and Langley Research Center, eds. Computer code for determination of thermally perfect gas properties. National Aeronautics and Space Administration, Langley Research Center, 1994.

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R, Edwards Jack, and NASA Glenn Research Center, eds. Numerical speed of sound and its application to schemes for all speeds. National Aeronautics and Space Administration, Glenn Research Center, 1999.

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R, Edwards Jack, and NASA Glenn Research Center, eds. Numerical speed of sound and its application to schemes for all speeds. National Aeronautics and Space Administration, Glenn Research Center, 1999.

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R, Millman Daniel, Greendyke Robert B, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Finite-differnce solution for laminar or turbulent boundary layer flow over axisymmetric bodies with ideal gas, CF, or equilibrium air chemistry. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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R, Millman Daniel, Greendyke Robert B, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Finite-difference solution for laminar or turbulent boundary layer flow over axisymmetric bodies with ideal gas, CF,́ or equilibrium air chemistry. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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R, Millman Daniel, Greendyke Robert B, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Finite-differnce solution for laminar or turbulent boundary layer flow over axisymmetric bodies with ideal gas, CF, or equilibrium air chemistry. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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W, Paulson John, Weilmuenster K. James, and United States. National Aeronautics and Space Administration., eds. Experimental and computational analysis of shuttle orbiter hypersonic trim anomaly. American Institute of Aeronautics and Astronautics, 1995.

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R, Spall John, and Langley Research Center, eds. Time-dependent solution for axisymmetric flow over a blunt body with ideal gas, CF,□ or equilibrium air chemistry. National Aeronautics and Space Administration, Langley Research Center, 1987.

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Book chapters on the topic "Ideal gas flow"

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Boldrighini, C., A. Masi, A. Nogueria, and E. Presutti. "The Dynamics of a Particle Interacting with a Semi-Infinite Ideal Gas is a Bernoulli Flow." In Statistical Physics and Dynamical Systems. Birkhäuser Boston, 1985. http://dx.doi.org/10.1007/978-1-4899-6653-7_10.

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Matar, C., P. Cinnella, X. Gloerfelt, S. Sundermeier, L. Hake, and S. aus der Wiesche. "Numerical Investigation of the Transonic Non-ideal Gas Flow Around a Circular Cylinder at High Reynolds Number." In Direct and Large Eddy Simulation XIII. Springer Nature Switzerland, 2023. http://dx.doi.org/10.1007/978-3-031-47028-8_25.

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

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Sahu, P. K. "Unsteady Flow Behind an MHD Exponential Shock Wave in a Rotational Axisymmetric Non-ideal Gas with Conductive and Radiative Heat Fluxes." In Learning and Analytics in Intelligent Systems. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-42363-6_121.

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Sahu, P. K. "Similarity Solution for the Flow Behind an Exponential Shock Wave in a Rotational Axisymmetric Non-ideal Gas Under the Influence of Gravitational Field with Conductive and Radiative Heat Fluxes." In Learning and Analytics in Intelligent Systems. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-42363-6_122.

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Chassaing, Patrick. "One-Dimensional Steady Flows of an Ideal Compressible Gas." In Fundamentals of Fluid Mechanics. Springer International Publishing, 2022. http://dx.doi.org/10.1007/978-3-031-10086-4_8.

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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. Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-69306-0_8.

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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. Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-69306-0_15.

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Shi, Y. H., and J. Y. Yang. "High Resolution Quantum Kinetic Beam Schemes and Its Applications to Ideal Quantum Gas Dynamical Flows." In Computational Fluid Dynamics 2006. Springer Berlin Heidelberg, 2009. http://dx.doi.org/10.1007/978-3-540-92779-2_29.

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Schuster, D., Y. Ince, Alexis Giauque, and Christophe Corre. "Assessment of Density and Compressibility Corrections for RANS Simulations of Real Gas Flows Using SU2." In Proceedings of the 4th International Seminar on Non-Ideal Compressible Fluid Dynamics for Propulsion and Power. Springer Nature Switzerland, 2023. http://dx.doi.org/10.1007/978-3-031-30936-6_9.

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Conference papers on the topic "Ideal gas flow"

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Arona, Adam, Guo-Xiang Wang, and Vish Prasad. "CLOSED-FORM SOLUTION FOR THE COMPRESSIBLE FLOW OF IDEAL GAS IN A PIPE WITH BOTH FRICTION AND HEAT TRANSFER." In 10th Thermal and Fluids Engineering Conference (TFEC). Begellhouse, 2025. https://doi.org/10.1615/tfec2025.fnd.056034.

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Carlson, Jan-Renee. "Assessment of Using Ideal Gas for Predicting Boattail Flow at Cryogenic Temperatures." In AIAA SCITECH 2023 Forum. American Institute of Aeronautics and Astronautics, 2023. http://dx.doi.org/10.2514/6.2023-2275.

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Semikolenov, Andrey V. "Molecular flow of an ideal gas through a small hole channel into a vacuum." In INTERNATIONAL CONFERENCE ON INFORMATICS, TECHNOLOGY, AND ENGINEERING 2021 (InCITE 2021): Leveraging Smart Engineering. AIP Publishing, 2022. http://dx.doi.org/10.1063/5.0074748.

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Semikolenov, Andrey V. "Molecular flow of an ideal gas through a small hole channel into a vacuum." In INTERNATIONAL CONFERENCE ON INFORMATICS, TECHNOLOGY, AND ENGINEERING 2021 (InCITE 2021): Leveraging Smart Engineering. AIP Publishing, 2022. http://dx.doi.org/10.1063/5.0074748.

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Kajasa, Bojan, Michael Lockan, and Eberhard Nicke. "Steam compressor flow simulation close to the saturation line using non-ideal gas model." In GPPS Chania24. GPPS, 2024. http://dx.doi.org/10.33737/gpps24-tc-077.

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The heat supply for industrial production in the medium temperature range can be provided by green electricity to substitute fossil energy sources. Here the use of High-Temperature Heat-Pumps (HTHP) is a very promising technology to reduce significantly the power demand. The operation of the HTHP require a dedicated design of the turbomachinary used within. For the working medium low superheated steam a well-adapted non-ideal gas model is required for the 3DRANS simulations. In addition to the temperature dependence, a model adaptation is developed to include the pressure dependence of the gas
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Ozalp, Nesrin, Vidyasagar Shilapuram, and D. Jayakrishna. "Modeling of Vortex-Flow Solar Reactor via Ideal Reactors in Series Approach." In ASME 2010 4th International Conference on Energy Sustainability. ASMEDC, 2010. http://dx.doi.org/10.1115/es2010-90324.

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In this work, we present a thorough reaction engineering analysis on the modeling of a vortex-flow reactor to show that commonly practiced one-plug reactor approach is not sufficient to explain the flow behavior inside the reactor. Our study shows that N-plug flow reactors in series is the best approach in predicting the flow dynamics based on the computational fluid dynamics (CFD) simulations. We have studied the residence time distribution using CFD by two different methods. The residence time distribution characteristics are calculated by approximating the real reactor as N-ideal reactors i
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Nie, Laixiao, Dandan Zheng, Tao Zhang, Xiaoli Guo, and Heming Hu. "The measurement performance of multi-path gas ultrasonic flowmeter in the non-ideal flow field." In 2012 2nd International Conference on Consumer Electronics, Communications and Networks (CECNet). IEEE, 2012. http://dx.doi.org/10.1109/cecnet.2012.6202054.

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Jaiswal, Abhijeet, Ashwin S. Dhoble, and D. J. Tidke. "High Compressible Flow Through Jet Blast Deflector." In ASME 2017 Gas Turbine India Conference. American Society of Mechanical Engineers, 2017. http://dx.doi.org/10.1115/gtindia2017-4699.

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Jet blast impact on aerofoil blade of the deflector is studied which redirects the high energy exhaust of jet engine during the ground testing. The geometric model of aerofoils is designed with structured mesh around the aerofoil in rectangular domain generated in ICEM 16 software. The jet blast impact on aerofoil blade of the deflector is numerically simulated with SST k-ω model based on CFD theory. The fluid flow is high-speed compressible flow and flowing fluid air is considered as an ideal gas and also Sutherland’s law viscosity is applied to account for the dependence of molecular viscosi
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Chai, D., Z. Fan, and X. Li. "A Unified Convection-Diffusion Layered Model For Non-Ideal Rarefied Gas Flow In Nanoscale Porous Media." In ECMOR XVI - 16th European Conference on the Mathematics of Oil Recovery. EAGE Publications BV, 2018. http://dx.doi.org/10.3997/2214-4609.201802205.

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Hendricks, Gavin J., Jayant S. Sabnis, and Matthew R. Feulner. "Analysis of Instability Inception in High-Speed Multi-Stage Axial-Flow Compressors." In ASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition. American Society of Mechanical Engineers, 1996. http://dx.doi.org/10.1115/96-gt-360.

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A nonlinear, two-dimensional, compressible dynamic model has been developed to study rotating stall/surge inception and development in high speed, multi-stage, axial flow compressors. The flow dynamics are represented by the unsteady Euler equations, solved in each interblade row gap and inlet and exit ducts as two-dimensional domains, and in each blade passage as a one-dimensional domain. The resulting equations are solved on a computational grid. The boundary conditions between domains are represented by ideal turning coupled with empirical loss and deviation correlations. Results are presen
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Reports on the topic "Ideal gas flow"

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Kirkpatrick, Mitchell, and Willson. L51953 CFD Modeling of Gas Flow and Mixing in a Two-Stroke Natural Gas Engine. Pipeline Research Council International, Inc. (PRCI), 2002. http://dx.doi.org/10.55274/r0010912.

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The objective of this project is to examine the effect of the injection pressure on the subsequent mixing in the cylinder. We examine the injection of natural gas from two types of poppet valves, shrouded and unshrouded valves and assess the ability of a commercial CFD code to compute the velocity and pressure profiles in high pressure gas flow from simple sonic nozzles. A sonic nozzle is a convergent or straight nozzle with an exit Mach number equal to one. The main parameters determining the type of the flow exiting from a sonic nozzle are the ratio of the injection pressure to the cylinder
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George. PR-015-05602-R01 Evaluation of Clamp-on Ultrasonic Meters as Diagnostic Tools. Pipeline Research Council International, Inc. (PRCI), 2008. http://dx.doi.org/10.55274/r0011135.

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This study has evaluated the ability of commercially available clamp-on ultrasonic meters (USMs) to diagnose natural gas flow conditions that can produce measurement errors in traditional natural gas meters, and quantify the errors in measurements made with traditional metering technologies under these conditions. Commercially available clamp-on meters were tested in a fully developed, steady flow downstream of a high-performance flow conditioner to evaluate their measurement repeatability and reproducibility. The clamp-on meters were then installed on a conventional orifice meter run and an i
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Witte and Grant. PR-015-14600-R01 New Generation USM in Compact Installations Without Flow Conditioners. Pipeline Research Council International, Inc. (PRCI), 2015. http://dx.doi.org/10.55274/r0010824.

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Certain new ultrasonic meter designs in were evaluated in compact installations. The natural gas industry is interested in realizing possible capital cost savings that would be achieved if ultrasonic meters could be installed in a configuration using meter tube lengths that are shorter than those commonly used today. As a starting point for this study, the short- and close-coupled installation details described in American Gas Association Report 7, �Measurement of Gas by Turbine Meters,� were accepted as reasonable short dimension installations to be studied. This document reports on the test
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Vieira, Greg, and Daniel Olsen. PR179-22206-R01 Prechamber Air and Fuel Premixing Proof of Concept. Pipeline Research Council International, Inc. (PRCI), 2024. http://dx.doi.org/10.55274/r0000099.

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This study investigates the feasibility of injecting a premixed air and fuel charge into the precombustion chamber (PCC) of a Cooper-Bessemer GMV-4TF 2-stroke lean-burn natural gas engine. The primary ob-jectives are to enhance combustion stability, reduce emissions, and address the challenges associated with stratification within the PCC. Computational fluid dynamics (CFD) simulations were conducted to evaluate both ideal and practical premixed scenarios. The ideal premixed scenario aimed to achieve improved ho-mogeneity and faster flame propagation. Low-pressure premixed injections were test
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Sridhar, Song, and Nored. L52227 Guidelines-Quality Standards for Transportation of Gas Containing Mixed Corrosive Constituents. Pipeline Research Council International, Inc. (PRCI), 2004. http://dx.doi.org/10.55274/r0010901.

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Gas quality specifications are set for commercial considerations and are influenced by several engineering factors including preventing corrosion, preventing blockages from freezing and hydrates, and the heating value of the gas. The Office of Pipeline Safety (OPS) Enforcement Manual for internal corrosion control states that the operator should have a procedure to determine if the gas is corrosive. Violation exists if (1) the corrosive potential of the gas is not determined by appropriate tests, and (2) suitable monitoring methods are not used to determine the effectiveness of steps taken to
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Banji, Titilope, and Daniel Olsen. PR-179-22207-R01 Improved In-Cylinder Mixing Injection Pressure Sensitivity. Pipeline Research Council International, Inc. (PRCI), 2024. http://dx.doi.org/10.55274/r0000063.

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Large-bore, natural gas-fueled engines are used for gas compression at over 1700 compression stations across the US, and methane emissions have presented a challenge to their optimization over the years. A significant root of this problem has been linked to the level of air-fuel mixing in the main combustion chamber of these engines as poor mixing results in low combustion efficiency. High-pressure fuel injection is believed to be a significant way to improve air-fuel mixing in natural gas engine combustion chambers. The purpose of this present study is to determine the sensitivity of in-cylin
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Thompson and Lawson. L51691 Fracture Control Technology for Natural Gas Pipelines. Pipeline Research Council International, Inc. (PRCI), 1993. http://dx.doi.org/10.55274/r0011368.

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Operational integrity of gas-transmission pipelines is a goal of all operators. Pipeline integrity is achieved by planning, controlling, and monitoring a number of elements, all of which contribute to the total pipeline system integrity. Elements that affect overall pipeline integrity are pipeline design, pipe specification, pipe transportation and handling, pipeline construction and inspection, preservice testing, and operation and maintenance practices. Fracture control is part of a number of these elements. This research report and software satisfies the industry need for a comprehensive de
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Snyder, Victor A., Dani Or, Amos Hadas, and S. Assouline. Characterization of Post-Tillage Soil Fragmentation and Rejoining Affecting Soil Pore Space Evolution and Transport Properties. United States Department of Agriculture, 2002. http://dx.doi.org/10.32747/2002.7580670.bard.

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Tillage modifies soil structure, altering conditions for plant growth and transport processes through the soil. However, the resulting loose structure is unstable and susceptible to collapse due to aggregate fragmentation during wetting and drying cycles, and coalescense of moist aggregates by internal capillary forces and external compactive stresses. Presently, limited understanding of these complex processes often leads to consideration of the soil plow layer as a static porous medium. With the purpose of filling some of this knowledge gap, the objectives of this Project were to: 1) Identif
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Soramäki, Kimmo. Financial Cartography. FNA, 2019. http://dx.doi.org/10.69701/ertx8007.

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Geographic maps have been of military and economic importance throughout the ages. Rulers have commissioned maps to control the financial, economic, political, and military aspects of their sovereign entities. Large scale projects like the Ordnance Survey in the UK in the late 18th century, and the Lewis and Clark Expedition a few decades later to map the American West, are early examples of trailblazing efforts to create accurate modern maps of high strategic importance. Digitalization, globalization, and a larger urban and educated workforce necessitate a new understanding of the world, beyo
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Crispin, Darla. Artistic Research as a Process of Unfolding. Norges Musikkhøgskole, 2018. http://dx.doi.org/10.22501/nmh-ar.503395.

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Abstract:
As artistic research work in various disciplines and national contexts continues to develop, the diversity of approaches to the field becomes ever more apparent. This is to be welcomed, because it keeps alive ideas of plurality and complexity at a particular time in history when the gross oversimplifications and obfuscations of political discourses are compromising the nature of language itself, leading to what several commentators have already called ‘a post-truth’ world. In this brutal environment where ‘information’ is uncoupled from reality and validated only by how loudly and often it is
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