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1983
In the area of inviscid compressible flows there are a variety of practical problems that arise in everyday engineering applications. These include rocket nozzle flows, aircraft and missile engine inlet flows, reentry vehicle and rocket aerodynamics, blast fields generated by different types of energy release, and aircraft flow fields.
Roger Peyret, Thomas D. Taylor
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In the area of inviscid compressible flows there are a variety of practical problems that arise in everyday engineering applications. These include rocket nozzle flows, aircraft and missile engine inlet flows, reentry vehicle and rocket aerodynamics, blast fields generated by different types of energy release, and aircraft flow fields.
Roger Peyret, Thomas D. Taylor
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Intermittency in Compressible Flows
1998We determine scaling exponents of structure functions for a computation with the Piecewise Parabolic Method [1] (or PPM) of a compressible flow at a r.m.s. Mach number of unity, using periodic boundary conditions and 5123 grid points, with δx the uniform grid increment. In [2] were analyzed similar computations with a one-dimensional shear wave forcing,
Paul R. Woodward +2 more
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2018
Selected phenomena associated with fluid compressibility, and the methods which are used to obtain quantitative descriptions of compressible flows, are discussed in this chapter. For simplicity, the viscous effect is neglected, while the compressible effect, which is a measure of the inertial effect, is taken into account due to its significant ...
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Selected phenomena associated with fluid compressibility, and the methods which are used to obtain quantitative descriptions of compressible flows, are discussed in this chapter. For simplicity, the viscous effect is neglected, while the compressible effect, which is a measure of the inertial effect, is taken into account due to its significant ...
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2017
Abstract In this chapter gas flow through pipes is analysed, taking account of compressibility and either friction or heat exchange with the fluid. It is shown that in all cases the key parameter is the Mach number. The analyses are based upon the conservation laws for mass, momentum, and energy, together with an equation of state.
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Abstract In this chapter gas flow through pipes is analysed, taking account of compressibility and either friction or heat exchange with the fluid. It is shown that in all cases the key parameter is the Mach number. The analyses are based upon the conservation laws for mass, momentum, and energy, together with an equation of state.
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A-to-Z Guide to Thermodynamics, Heat and Mass Transfer, and Fluids Engineering, 2006
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Computational Methods for Fluid Dynamics, 2019
J. Ferziger, M. Peric, R. Street
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J. Ferziger, M. Peric, R. Street
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An improved ghost‐cell immersed boundary method for compressible flow simulations
, 2017Cheng Chi, B. Lee, H. Im
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3D reconstruction of a compressible flow by synchronized multi-camera BOS
, 2017F. Nicolas +5 more
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Implementation of a Compressible-Flow Simulation Code in the D Programming Language
, 2016P. Jacobs, R. Gollan
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