NASA Technical Reports Server (NTRS) : Numerical pdf

NASA Technical Reports Server (NTRS) : Numerical_bookcover

NASA Technical Reports Server (NTRS) : Numerical

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An exact nonlinear mathematical model that accounts for three-dimensional cascade effects about the inner portions of the rotor blades and compressibility effects about the tip regions of the blades was derived. An artificially time dependent version was iteratively solved by a finite volume technique involving an artificial viscosity and a three-level consecutive mesh refinement. The exact boundary conditions were applied by generating a boundary conforming periodic computation mesh

  • Creator/s: NASA Technical Reports Server (NTRS
  • Date: 1/1/1980
  • Year: 1980
  • Book Topics/Themes: NASA Technical Reports Server (NTRS), COMPRESSIBLE FLOW, INVISCID FLOW, ROTOR AERODYNAMICS, TURBINE BLADES, WINDPOWERED GENERATORS, AIRFOIL PROFILES, CASCADE FLOW, MATHEMATICAL MODELS, NONLINEAR SYSTEMS, THREE DIMENSIONAL FLOW, Dulikravich, D. S

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