This is the authors' abstract. We don't add key points for this paper.
T viscous drag of turbulent boundary layers is a significant factor contributing to the fuel costs of the airlines. Several studies have indicated that microsurface geometry variations which change the near-wall structure of the flow have been effective in reducing drag. Summarized here is an investigation into the verification and extension of the most promising of these riblet variations.
Answers are grounded in this paper and cite their sources.
No takes yet. Share an insight, caveat, or question.
Michael J. Walsh (1983) studied this question.
Synapse has enriched 10 related papers. Consider them for comparative context: