Model of Distributed Receptivity to Kinetic Fluctuations in High-Speed Boundary Layers-Reference-Cited by-同舟云学术

Model of Distributed Receptivity to Kinetic Fluctuations in High-Speed Boundary Layers

Published:2019-11 Issue:11 Volume:57 Page:4750-4763
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Edwards Luke D.¹,Tumin Anatoli¹

Affiliation:

1. The University of Arizona, Tucson, Arizona 85721

Funder

Air Force Office of Scientific Research

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/am-pdf/10.2514/1.J058432

Reference49 articles.

1. MorkovinM. V. “Critical Evaluation of Transition from Laminar to Turbulent Shear Layers with Emphasis on Hypersonically Travelling Bodies,” U.S. Air Force Flight Dynamics Lab. AFFDL-TR 68–149, Wright Patterson Air Force Base, OH, 1969.

2. Boundary-Layer Stability and Transition

3. MackL. M. “Transition and Laminar Instability,” NASA, CP-153203, 1977.

4. Boundary-layer receptivity to acoustic disturbances

5. Generation of Tollmien–Schlichting waves by convecting gusts interacting with sound

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