Step Excrescence Effects for Manufacturing Tolerances on Laminar Flow Wings-Reference-Cited by-同舟云学术

Step Excrescence Effects for Manufacturing Tolerances on Laminar Flow Wings

Published:2010-01-04 Issue: Volume: Page:
ISSN:
Container-title:48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
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Author:

Drake Aaron¹,Bender Anne¹,Korntheuer Andrea¹,Westphal Russell²,Rohe Wayne³,Dale Gary³,McKeon Beverley⁴,Geraschchenko Sergiy⁴

Affiliation:

1. Northrop Grumman Corporation

2. California Polytechnic State University

3. U.S. Air Force Research Laboratory

4. California Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-375

Reference11 articles.

1. 1Fage, A.TheSmallestSizeofaSpanwiseSurfaceCorrugationwhichAffectsBoundary-LayerTransitiononanAerofoil,‖ RAE R&M 2120,January1943.

2. 2Drake, A., Westphal, R. V., Zuniga, F. A., Kennelly, R. A., and Koga, D. J.Wing Leading Edge Joint Laminar Flow Tests,‖ NASATM4762,1996.

3. 3Driver, D. M., and Drake, A.Skin Friction Measurements Using Oil Film Interferometry in the 11' Transonic Wind TunnelatAmes,‖ AIAA-2004-1359,42ndAIAAAerospaceSciencesMeeting,Jan.2004.

4. 4Braslow, A. L.Review of the Effect of Distributed Surface Roughness on Boundary Layer Transition‖ AGARD Report 254,1960.

5. 5Smith, A. M. O.,and Clutter, D. W.The Smallest Height ofRoughness Capable ofAffectingBoundary-Layer Transition in Low-Speed Flow‖ Douglas Aircraft Co.EngineeringReportES26803,1954.

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