Wall-Pressure Sources Near an Airfoil Trailing Edge Under Separated Laminar Boundary Layers
Author:
Affiliation:
1. University of Cambridge, Cambridge, England CB3 ODY, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J050477
Reference56 articles.
1. A Prediction Model for Separated-Flow Transition
2. A Bypass Transition Model for Boundary Layers
3. Transition Length Prediction for Flows With Rapidly Changing Pressure Gradients
4. Measurements in Separated and Transitional Boundary Layers Under Low-Pressure Turbine Airfoil Conditions
5. Measurements in a separation bubble on an airfoil using laser velocimetry
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