Effects of Shock-Tube Cleanliness on Hypersonic Boundary Layer Transition at High Enthalpy-Reference-Cited by-同舟云学术

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Effects of Shock-Tube Cleanliness on Hypersonic Boundary Layer Transition at High Enthalpy

Published:2017-01 Issue:1 Volume:55 Page:332-338
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Jewell Joseph S.¹,Parziale Nicholaus J.²,Leyva Ivett A.³,Shepherd Joseph E.⁴

Affiliation:

1. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433

2. Stevens Institute of Technology, Hoboken, New Jersey 07030

3. U.S. Air Force Office of Scientific Research, Arlington Air Force Base, Virginia 22203

4. California Institute of Technology, Pasadena, California 91125

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J054897

Reference43 articles.

1. Notes on Initial Disturbance Fields for the Transition Problem

2. Effects of High-Speed Tunnel Noise on Laminar-Turbulent Transition

3. Hypersonic laminar–turbulent transition on circular cones and scramjet forebodies

4. Development of Hypersonic Quiet Tunnels

5. High-Bandwidth Optical Measurements of the Second-Mode Instability in a Mach 6 Quiet Tunnel

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1. Improved Debris Blocker and Flow Terminator in a Shock Tunnel;AIAA SCITECH 2024 Forum;2024-01-04

2. High-Enthalpy, Hypersonic Aerodynamic Validation Study with Multiple Physics-Fidelity Models;AIAA SCITECH 2024 Forum;2024-01-04

3. Characterization Progress of an Absorption Laser Differential Interferometer;AIAA SCITECH 2024 Forum;2024-01-04

4. Numerical study on the role of aerosol particles in hypersonic boundary layer transition;AIAA SCITECH 2024 Forum;2024-01-04

5. Freestream Temperature Effects on the Receptivity of Hypersonic Boundary Layer Induced by Finite-Amplitude Pulse Entropy Waves;Journal of Applied Fluid Mechanics;2023-12-01

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