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An examination of the behaviour of aerofoils in unsteady flow with special reference to the Kutta condition

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posted on 26.10.2020, 16:08 by P. Royle
An examination of the behaviour of aerofoils in unsteady flow with special reference to the Kutta condition

Funding

Loughborough University of Technology

Great Britain, National Gas Turbine Establishment

United States, NASA

History

School

  • Aeronautical, Automotive, Chemical and Materials Engineering

Department

  • Aeronautical and Automotive Engineering

Publisher

Loughborough University of Technology

Rights holder

© P. Royle

Publication date

1977

Notes

A Master's Thesis. Submitted in partial fulfilment of the requirements for the award of the degree of Master of Science of Loughborough University of Technology.

Language

en

Supervisor(s)

M.V. Lowson ; D.L. Hawkings ; F.G. Maccabee

Qualification name

MSc

Qualification level

Masters

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