Three-dimensional shear-driven boundary-layer flow with streamwise adverse pressure gradient
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California
2. Naval Postgraduate School, Monterey, California
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.10322
Reference12 articles.
1. Measurements in the turbulent boundary layer on an ‘infinite’ swept wing
2. Experimental study of a three-dimensional, shear-driven, turbulent boundary layer
3. The structure of a separating turbulent boundary layer. Part 1. Mean flow and Reynolds stresses
4. Measurements in a three-dimensional turbulent boundary layer induced by a swept, forward-facing step
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