Second Mode Suppression in Hypersonic Boundary Layer by Roughness: Design and Experiments-Reference-Cited by-同舟云学术

Second Mode Suppression in Hypersonic Boundary Layer by Roughness: Design and Experiments

Published:2015-10 Issue:10 Volume:53 Page:3138-3144
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Fong Kahei Danny,Wang Xiaowen,Huang Yuet,Zhong Xiaolin,McKiernan Gregory R.,Fisher Roy A.,Schneider Steven P.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J054100

Reference28 articles.

1. Summary of Hypersonic Boundary-Layer Transition Experiments on Blunt Bodies with Roughness

2. BOUNDARY-LAYER RECEPTIVITY TO FREESTREAM DISTURBANCES

3. JamesC. S. “Boundary Layer Transition on Hollow Cylinders in Supersonic Free Flight as Affected by Mach Number and a Screwthread Type of Surface Roughness,” NASA TR-Memo-1-20-59A, 1959.

4. HollowayP. F.SterrettJ. R. “Effect of Controlled Surface Roughness on Boundary-Layer Transition and Heat Transfer at Mach Numbers of 4.8 and 6.0, ” NASA TN-D-2054, 1964.

5. Experiment of the Two-Dimensional Roughness Effect on Hypersonic Boundary-Layer Transition

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