Transition due to Surface Steps in the Presence of Favorable Pressure Gradients
Author:
Affiliation:
1. Northrop Grumman Corporation
2. Washington State University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-7334
Reference12 articles.
1. 1A. Fage, "The smallest size of a spanwise surface corrugation which affects boundary-layer transition on an aerofoil," RAE R&M 2120,January1943.
2. 3D.M. Driver and A. Drake, "Skin friction measurements using oil film interferometry in the 11' transonic wind tunnel at Ames," AIAA-2004-1359, January2004.
3. An Approach to Measuring the Effects of Surface Excrescences on Transition in the Presence of Arbitrary Pressure Gradients
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