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Supersonic laminar flow control studies in the SUPERTRAC project
KTH, School of Engineering Sciences (SCI).
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2006 (English)In: ICAS-Secretariat, 2006, 1014-1023 p.Conference paper, Published paper (Refereed)
Abstract [en]

The global objective of the SUPERTRAC project is to explore the possibilities to delay laminar-turbulent transition on supersonic aircraft wings. The following techniques are investigated: micron-sized roughness elements, anti-contamination devices, suction and shape optimization. This paper provides an overview of the project and describes in more detail the numerical investigations performed during the first year in order to design two wind tunnel models. These models will be used to assess the capabilities of the first three techniques listed above.

Place, publisher, year, edition, pages
2006. 1014-1023 p.
Series
ICAS-Secretariat - 25th Congress of the International Council of the Aeronautical Sciences 2006, 2
Keyword [en]
Boundary layer, Laminar flow control, Supersonic flow, Anti-contamination, First year, Global objective, Laminar-turbulent transition, Numerical investigations, Roughness elements, Wind tunnel models, Aerodynamics, Boundary layers, Flow control, Supersonic aircraft, Wings, Laminar flow
National Category
Fluid Mechanics and Acoustics
Identifiers
URN: urn:nbn:se:kth:diva-155039Scopus ID: 2-s2.0-84878460560ISBN: 9781604232271 (print)OAI: oai:DiVA.org:kth-155039DiVA: diva2:759458
Conference
25th Congress of the International Council of the Aeronautical Sciences 2006, 3 September 2006 through 8 September 2006, Hamburg
Note

QC 20141030

Available from: 2014-10-30 Created: 2014-10-29 Last updated: 2014-10-30Bibliographically approved

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