Influence of a Backward-Facing Step on Swept-Wing Boundary-Layer Transition-Reference-Cited by-同舟云学术

Influence of a Backward-Facing Step on Swept-Wing Boundary-Layer Transition

Published:2019-01 Issue:1 Volume:57 Page:267-278
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Eppink Jenna L.¹,Wlezien Richard W.²,King Rudolph A.¹,Choudhari Meelan¹

Affiliation:

1. NASA Langley Research Center, Hampton, Virginia 23681

2. Missouri University of Science and Technology, Rolla, Missouri 65409

Funder

National Aeronautics and Space Administration

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J057437

Reference20 articles.

1. Manufacturing Tolerances for Natural Laminar Flow Airframe Surfaces

2. FageA. “The Smallest Size of a Spanwise Surface Corrugation Which Affects Boundary Layer Transition on an Aerofoil,” British Aeronautical Research Council R&M 2120, London, 1943.

3. CarmichaelB. “Surface Waviness Criteria for Swept and Unswept Laminar Suction Wings,” Norair Rept. NOR-59-438 (BLC-123), Hawthorne, CA, 1959.

4. A Survey of the Effects of Small Protuberances on Boundary-Layer Flows

5. Boundary-Layer Transition

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