2023
DOI: 10.48550/arxiv.2302.09797
|View full text |Cite
Preprint
|
Sign up to set email alerts
|

Delaying transition induced by a strip of distributed roughness using additional fine grit roughness

Abstract: Distributed roughness occurs on aerodynamic surfaces like wind/gas turbine blades and aircraft wings causing early boundary layer transition resulting in higher skin friction, reduced lift-to-drag ratio, and lower power production. Despite being a recurring theme in practical engineering scenarios, the mechanism of boundary layer transition caused by distributed roughness is not well understood, and consequently, from a fluid dynamics perspective, methods for mitigating its effects are scarce. In this work, we… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...

Citation Types

0
0
0

Publication Types

Select...

Relationship

0
0

Authors

Journals

citations
Cited by 0 publications
references
References 34 publications
(67 reference statements)
0
0
0
Order By: Relevance

No citations

Set email alert for when this publication receives citations?