Summary
An experimental study on a swept wing is performed to determine the effects of boundary layer suction on the leading edge contamination. The results are compared with the direct numerical simulations of Spalart.
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References
Pfenninger, W., “Flow Phenomena at the Leading Edge of Swept Wings” -Recent Developments in Boundary Layer Research, Part IV — AGARDograph 97 (May 1965)
Arnal, D., “Boundary Layer Transition: Prediction, Application to Drag Reduction” - AGARD/FDP VKI Special Course on Skin Friction Drag Reduction, Brussels, Belgium (2–6 March 1992)
Reneaux, J., Preist, J., Arnal, D., Juillen, J.C., “Design and Testing of Two Gaster Bumps for the A320 Laminar Flow” - Internal Report (September 1992)
Spalart, P.R., “Direct Numerical Study of Leading Edge Contamination”, AGARD CP ∘ 438 (1988)
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© 1995 Springer-Verlag Berlin Heidelberg
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Juillen, J.C., Arnal, D. (1995). Experimental Study of Boundary Layer Suction Effects on Leading Edge Contamination along the Attachment Line of a Swept Wing. In: Kobayashi, R. (eds) Laminar-Turbulent Transition. IUTAM Symposia. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-79765-1_20
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DOI: https://doi.org/10.1007/978-3-642-79765-1_20
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-79767-5
Online ISBN: 978-3-642-79765-1
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