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Research article

First published 1999-6

Throughflow model for design and analysis integrated in a three-dimensional Navier-Stokes solver

A Sturmayr, Ch Hirsch

Proceedings of the Institution of Mechanical Engineers,Part A: Journal of Power and Energy

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Research article

First published 2021-12

A viscous blade body force model for computational fluid dynamics–based throughflow analysis of axial compressors

Jian Li, Jinfang Teng, Mingmin Zhu [...]

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Research article

First published 2016-2

A CFD-based throughflow method with an explicit body force model and an adaptive formulation for the S2 streamsurface

Roberto Pacciani, Filippo Rubechini, Michele Marconcini [...]

Proceedings of the Institution of Mechanical Engineers,Part A: Journal of Power and Energy

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Research article

First published 2019-11

Time-marching throughflow analysis of multistage axial compressors based on a novel inviscid blade force model

Chen Yang, Hu Wu, Jinguang Yang [...]

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Research article

First published 2021-4

The genetic algorithm-radial basis function neural network to quickly predict aerodynamic performance of compressors

Tianquan Tang, Bo Liu

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Research article

First published 2025

An inverse model for primary design parameter interaction of 1.5 stage counter-rotating turbine

Ben Zhao, Shilin Zhao, Shuo Liu [...]

Proceedings of the Institution of Mechanical Engineers,Part C: Journal of Mechanical Engineering Science

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Research article

First published 2022-6

Loss prediction of axial compressors using genetic algorithm–back propagation neural network in throughflow method

Jian Li, Jinfang Teng, Mingmin Zhu [...]

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Research article

First published 1984-11

The Effect of Droplet Size on the Flow in the Last Stage of a One-Third Scale Model Low-Pressure Turbine

C C Yeoh, J B Young

Proceedings of the Institution of Mechanical Engineers,Part A: Journal of Power and Energy

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Research article

First published 2008-9

Axisymmetric design of axial turbomachines: An inverse method introducing profile losses

S Rosa Taddei, F Larocca

Proceedings of the Institution of Mechanical Engineers,Part A: Journal of Power and Energy

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Research article

First published 2017-8

Flow and windage due to bolts on a rotating disc

Sulfickerali Noor Mohamed, John Chew, Nick Hills

Proceedings of the Institution of Mechanical Engineers,Part C: Journal of Mechanical Engineering Science

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