BiGlobal Stability of Shear Flows

Spanwise & Streamwise Analyses

Doctoral thesis (2018)

Authors

K.J. Groot Aerodynamics - Aerospace Engineering

Research Group

Aerodynamics (Aerospace Engineering) (TU Delft)

DOI: https://doi.org/10.4233/uuid:60ef07b2-00db-418b-9495-5a9baf6105df

Flow instability Measured base flows Micro-ramp Swept-wing boundary layer Crossflow instability Streamwise BiGlobal problem

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http://resolver.tudelft.nl/uuid:60ef07b2-00db-418b-9495-5a9baf6105df

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Published Date

2018

Language

English

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Faculty

Aerospace Engineering

Department

Flow Physics and Technology

Research Group

Aerodynamics

Abstract

Laminar-turbulent transition dictates an increase in skin friction. The resulting turbulent skin friction contributes to approximately 40% of the total drag of commercial aircraft. Reducing the turbulent flow region by postponing transition can therefore significantly reduce the carbon footprint and costs of flying. Transition prediction is required in order to do so, which depends on a detailed understanding of the transition process.

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