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Philipp Tewes
Researcher at University of Arizona
Publications - 17
Citations - 307
Philipp Tewes is an academic researcher from University of Arizona. The author has contributed to research in topics: Airfoil & Boundary layer. The author has an hindex of 8, co-authored 17 publications receiving 265 citations.
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Journal ArticleDOI
Discrete Sweeping Jets as Tools for Improving the Performance of the V-22
Roman Seele,Philipp Tewes,Rene Woszidlo,Michael A. McVeigh,Nathaniel J. Lucas,Israel Wygnanski +5 more
TL;DR: In this article, a V-22 wing/nacelle combination with discrete jets pointing in the direction of streaming and sweeping side to side along the span was used to delay flow separation.
Proceedings ArticleDOI
On the Use of Sweeping Jets to Augment the Lift of a Lambda-Wing
TL;DR: In this paper, a lambda wing model, based on an airfoil, but containing simple flaps augmented by sweeping jet actuators, was constructed and tested, and the purpose of these tests was to assess the efficacy of this method of separation control on a realistic wing configuration.
Journal ArticleDOI
Applying the Boundary-Layer Independence Principle to Turbulent Flows
TL;DR: In this article, velocities measured in turbulent boundary layers over yawed flat plates confirmed that the mean velocity profiles normal to the leading edge are proportional to the velocity profiles parallel to it, with a proportionality constant depending on the yaw angle.
Proceedings ArticleDOI
On the effect of sweep on separation control
TL;DR: In this article, the performance of a flapped wing based on a NACA 0012 airfoil section and equipped with a linear array of fluidic oscillators was investigated experimentally to assess the significance of wing sweep and aspect ratio on the efficiency of the actuation.
Journal ArticleDOI
The application of boundary layer independence principle to three-dimensional turbulent mixing layers
TL;DR: In this article, the authors re-examine the broader ramifications of boundary layer growth on a yawed flat plate and the attached flow direction near the trailing edge of a highly swept-back wing.