Abstract
The influence of a three-dimensional surface perturbation on the transitional boundary layer has been investigated experimentally. The perturbation height and longitudinal location relative to the leading edge have been varied to represent the effects of moving the location of a joint on a typical aerodynamic surface. The experimental results indicate that while, for most configurations tested, the presence of a surface perturbation reduces the transitional Reynolds number, there are potential benefits to be realised with careful positioning of the rivet joint, promoting an increase in the transition onset location of up to 5%.
Original language | English |
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Title of host publication | 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition |
DOIs | |
Publication status | Published - 2010 |
Event | 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition - Orlando, United States Duration: 4 Jan 2010 → 7 Jan 2010 |
Conference
Conference | 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition |
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Country/Territory | United States |
City | Orlando |
Period | 4/01/10 → 7/01/10 |
Keywords
- Aerodynamic surfaces
- Leading edge
- Potential benefits
- Surface perturbations
- Three-dimensional surface
- Transitional boundary layers
ASJC Scopus subject areas
- Aerospace Engineering