Computational and experimental investigation of annulus heat transfer with swirl

Kim, J.C.; Bennett, John D.C.

doi:10.2514/6.1992-4060

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1993

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“…For discretization, a hybrid differencing scheme (Spalding, 1972) was used with a control volume formulation." (Kim and Bennett, 1992) The reader is referred to this and to the other references for additional information about the numerical procedure.…”

Section: Introductionmentioning

confidence: 99%

A Three-Dimensional Navier-Stokes Calculation Applied to an Axial Compressor Rotor and Stator

Dring¹,

VanSeters

Zacharias

1993

Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery

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The objective of this paper is to apply a three-dimensional Navier-Stokes calculation to the second stage rotor and stator of a large scale compressor and to compare the computed results with measured data. The comparisons include: (1) airfoil and endwall surface streamlines, (2) radial-circumferential distributions of exit total pressure, (3) spanwise distributions of circumferentially averaged inlet and exit flow quantities, and (4) fullspan airfoil pressure distributions. This assessment demonstrates that the computational state-of-the-art has advanced to a point where calculations such as this can be applied with reasonable confidence in both design and analysis situations.

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Section: Introductionmentioning

confidence: 99%