A Compact, Self-Contained System for Boundary Layer Measurements in Flight
Author:
Affiliation:
1. Washington State University
2. Northrop Grumman Corporation
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-3828
Reference10 articles.
1. 1Marshall, L. A. "Boundary-Layer Transition Results From the F-16XL-2 Supersonic Laminar Flow Control Experiment," NASA TM-1999-209013,1999.
2. In-Flight Skin Friction Measurements Using Oil Film Interferometry
3. 3Bui, T. T., Oates, B. L., and Gonsalez, J. C. "Design and Evaluation of a New Boundary-Layer Rake for Flight Testing," NASA TM-2000-209014,2000.
4. 4Rae,W.H.Jr.,andPope,A.,Low-SpeedWindTunnelTesting,2nded.,Wiley,NewYork,1984.
5. 5Bleazard,M."AResearchInstrumentforBoundaryLayerMeasurementsinFlight,"M.S.Thesis,SchoolofMechanicaland Materials Engineering, WashingtonStateUniv.,Pullman, WA, 2006.
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