Flow modelling in supersonic flows over surfaces with large roughness heights

Master Thesis (2013)
Author(s)

H. van Pelt (TU Delft - Aerospace Engineering)

Contributor(s)

BW van Oudheusden – Mentor (TU Delft - Aerodynamics)

LJ Souverein – Mentor (TU Delft - Aerodynamics)

Ferry F.J. Schrijer – Mentor (TU Delft - Aerodynamics)

BTC Zandbergen – Mentor (TU Delft - Space Systems Egineering)

Faculty
Aerospace Engineering
Copyright
© 2013 Hilbert van Pelt
More Info
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Publication Year
2013
Language
English
Copyright
© 2013 Hilbert van Pelt
Graduation Date
21-11-2013
Awarding Institution
Delft University of Technology
Programme
Aerospace Engineering
Faculty
Aerospace Engineering
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Abstract

Flow over smooth surfaces has been studied ever since the start of aerodynamic research. Non-smooth irregularities in rough walled surfaces will impact on the flow and induce changes in friction and heat transfer. The term 'rough walled' encompasses a range of shapes, ranging from material roughness to wall profiles with heights up to the boundary layer thickness. The effect of material roughness has been studied extensively, but data on large roughness elements is scarce and case-specific, depending on flow conditions and roughness element shape.

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