Computational Investigation of Step Excrescence Sensitivity in a Swept-Wing Boundary Layer-Reference-Cited by-同舟云学术

Computational Investigation of Step Excrescence Sensitivity in a Swept-Wing Boundary Layer

Published:2017-03 Issue:2 Volume:54 Page:602-626
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Tufts Matthew W.¹,Reed Helen L.¹,Crawford Brian K.¹,Duncan Glen T.¹,Saric William S.¹

Affiliation:

1. Texas A&M University, College Station, Texas 77843

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C033892

Reference35 articles.

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2. Analysis for the Application of Hybrid Laminar Flow Control to a Long-Range Subsonic Transport Aircraft

3. Toward Practical Laminar Flow Control - Remaining Challenges

4. BraslowA. L.KnoxE. C. “Simlified Method for Determination of Critical Height of Distributed Roughness Particles for Boundary-Layer Transition at Mach Numbers from 0 to 5,” NACA TN 4363, 1958.

5. The Smallest Height of Roughness Capable of Affecting Boundary-Layer Transition

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