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Research article

First published 2022-2

Effect of radial inflow distortion on the performance of a highly loaded tandem stage

Amit Kumar, AM Pradeep

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

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Research article

First published 2020-6

The effect of inlet distortion on low bypass ratio turbofan engines

Vishwas Verma, Gursharanjit Singh, AM Pradeep

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

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Research article

First published 2026-3

Effect of inlet geometric distortion on the aerodynamic performance of a multistage compressor

Hong Xie, Guoming Zhu, Libo Wang [...]

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

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Research article

First published 2009-2

Tip injection as a means for rotating stall control in an axial flow fan

P B Salunkhe, V S R K Reddy, A M Pradeep

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

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Research article

First published 2007-1

Predicted and measured performance and stability of two variants of a military fan

R. B. Ginder, W. J. Calvert, P. R. Emmerson

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

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Research article

First published 2021-12

Design methodology of a highly loaded tandem rotor and its performance analysis under clean and distorted inflows

Amit Kumar, AM Pradeep

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

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Research article

First published 2023-9

Effect of bend-induced inlet distortion on a centrifugal compressor performance and stall inception

Peng Wang, Ben Zhao, Qingjun Zhao [...]

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

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Other

First published 2005-1

Effect of vane-rotor interaction on the unsteady flowfield downstream of a transonic high pressure turbine

R Dénos, G Paniagua

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

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Research article

First published 2018-11

Fan tonal noise from aircraft aeroengines with short intake: A study at approach

S Guérin, A Holewa

International Journal of Aeroacoustics

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Research article

First published 2006-7

Background Stripes Affect Apparent Speed of Rotation

Stuart Anstis, Hiroyuki Ito, Patrick Cavanagh

Perception

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