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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 2020-10-26, 16:08 authored 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

Administrator link

Usage metrics

    Aeronautical and Automotive Engineering Theses

    Categories

    Keywords

    Kutta conditionAerofoilsEngineering not elsewhere classified

    Licence

    CC BY-NC 4.0

    Exports

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