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1Spectral methods

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“Spectral methods” Metadata:

  • Title: Spectral methods
  • Authors:
  • Language: English
  • Number of Pages: Median: 597
  • Publisher: Springer
  • Publish Date:
  • Publish Location: Berlin - London

“Spectral methods” Subjects and Themes:

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Access and General Info:

  • First Year Published: 2007
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: Unclassified

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    Compressible flow

    Compressible flow (or gas dynamics) is the branch of fluid mechanics that deals with flows having significant changes in fluid density. While all flows

    Aerodynamics

    technologies. Recent work in aerodynamics has focused on issues related to compressible flow, turbulence, and boundary layers and has become increasingly computational

    Bernoulli's principle

    incompressible flows (e.g. most liquid flows and gases moving at low Mach number). More advanced forms may be applied to compressible flows at higher Mach

    Dynamic pressure

    extended to include compressible flows. For compressible flow the isentropic relations can be used (also valid for incompressible flow): q = p s ( 1 + γ

    Mach number

    naturally when the continuity equation is nondimensionalized for compressible flows. If density variations are related to pressure through the isentropic

    Euler equations (fluid dynamics)

    conductivity. The Euler equations can be applied to incompressible and compressible flows. The incompressible Euler equations consist of Cauchy equations for

    Stagnation pressure

    incompressible flow shows that the stagnation pressure is equal to the dynamic pressure and static pressure combined. In compressible flows, stagnation pressure

    Orifice plate

    flow rates than the coefficients of conical-entrance and quarter-circle plates, especially at low flows and high viscosities. For compressible flows such

    Isentropic nozzle flow

    and the velocity of the flow will increase. However, as the speed of the flow approaches the speed of sound, compressibility effects on the gas are to

    Transonic

    disturbances within the flow are relatively small, which allows mathematicians and engineers to linearize the compressible flow equations into a relatively