Prediction Methodology for Second-Mode-Dominated Boundary-Layer Transition in Wind Tunnels-Reference-Cited by-同舟云学术

Prediction Methodology for Second-Mode-Dominated Boundary-Layer Transition in Wind Tunnels

Published:2017-02 Issue:2 Volume:55 Page:484-499
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Marineau Eric C.¹

Affiliation:

1. Arnold Engineering Development Complex, Silver Spring, Maryland 20903

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J055061

Reference18 articles.

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

2. PateS. “Dominance of Radiated Aerodynamic Noise on Boundary-Layer Transition in Supersonic/Hypersonic Wind Tunnels,” Arnold Engineering Development Center TR-77-107, Arnold Air Force Base, TN, 1978.

3. Mach 10 Boundary Layer Transition Experiments on Sharp and Blunted Cones (Invited)

4. Investigation of Mach 10 Boundary Layer Stability of Sharp Cones at Angle-of-Attack, Part 1: Experiments

5. Laminar boundary layer stability experiments on a cone at Mach 8. I - Sharp cone

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